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Complex Structures for Manned/Unmanned Aerial Vehicles

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Ridgard, Chris, Advanced Composites Group, Inc.; After several years of effort, a new generation of out of autoclave processable resin systems has been developed which it is believed will replace older oven vacuum bag cure (OVBC) resins such as the Advanced Composites Group, Inc.

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									AFRL-RX-WP-TM-2008-4054
COMPLEX STRUCTURES FOR MANNED/UNMANNED AERIAL VEHICLES Delivery Order 0019: Low Temp Composite Processing Mechanical Property Data
Chris Ridgard

Advanced Composites Group, Inc.

JANUARY 2008 Final Report

Approved for public release; distribution unlimited.
See additional restrictions described on inside pages

STINFO COPY

AIR FORCE RESEARCH LABORATORY MATERIALS AND MANUFACTURING DIRECTORATE WRIGHT-PATTERSON AIR FORCE BASE, OH 45433-7750 AIR FORCE MATERIEL COMMAND UNITED STATES AIR FORCE

NOTICE AND SIGNATURE PAGE

Using Government drawings, specifications, or other data included in this document for any purpose other than Government procurement does not in any way obligate the U.S. Government. The fact that the Government formulated or supplied the drawings, specifications, or other data does not license the holder or any other person or corporation; or convey any rights or permission to manufacture, use, or sell any patented invention that may relate to them. This report was cleared for public release by the Wright-Patterson Air Force Base (WPAFB) Public Affairs Office and is available to the general public, including foreign nationals. Copies may be obtained from the Defense Technical Information Center (DTIC) (http://www.dtic.mil).
THIS REPORT HAS BEEN REVIEWED AND IS APPROVED FOR PUBLICATION IN ACCORDANCE WITH ASSIGNED DISTRIBUTION STATEMENT.

*//signature// ________________________________________ TARA STORAGE, Program Engineer Composite and Hybrid Material Branch Nonmetallic Materials Division

//signature// _______________________________________ KEITH BOWMAN, Acting Chief Composite and Hybrid Materials Branch Nonmetallic Materials Division

//signature// ______________________________________ SHASHI K. SHARMA, Acting Deputy Chief Nonmetallic Materials Division Materials and Manufacturing Directorate

This report is published in the interest of scientific and technical information exchange, and its publication does not constitute the Government’s approval or disapproval of its ideas or findings.
*Disseminated copies will show “//signature//” stamped or typed above the signature blocks.

REPORT DOCUMENTATION PAGE

Form Approved OMB No. 0704-0188

The public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THE ABOVE ADDRESS.

1. REPORT DATE (DD-MM-YY)

2. REPORT TYPE

3. DATES COVERED (From - To)

January 2008
4. TITLE AND SUBTITLE

Final

14 September 2006 – 14 December 2007
5a. CONTRACT NUMBER

COMPLEX STRUCTURES FOR MANNED/UNMANNED AERIAL VEHICLES Delivery Order 0019: Low Temp Composite Processing Mechanical Property Data

FA8650-05-D-5807-0019
5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER

62102F
6. AUTHOR(S) 5d. PROJECT NUMBER

4347 Chris Ridgard
5e. TASK NUMBER

32
5f. WORK UNIT NUMBER

32300002
7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION REPORT NUMBER

Advanced Composites Group, Inc. 5350 South, 129th East Avenue Tulsa, OK 74134
9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/MONITORING AGENCY ACRONYM(S)

Air Force Research Laboratory Materials and Manufacturing Directorate Wright-Patterson Air Force Base, OH 45433-7750 Air Force Materiel Command United States Air Force
12. DISTRIBUTION/AVAILABILITY STATEMENT

AFRL/RXBC
11. SPONSORING/MONITORING AGENCY REPORT NUMBER(S)

AFRL-RX-WP-TM-2008-4054

Approved for public release; distribution unlimited.
13. SUPPLEMENTARY NOTES

PAO case number WPAFB 07-0682, 11 December 2007. Report contains color.
14. ABSTRACT

After several years of effort, a new generation of out of autoclave processable resin systems has been developed which it is believed will replace older oven vacuum bag cure (OVBC) resins such as the Advanced Composites Group, Inc. (ACG) LTM45EL material. The first of these new resins, MTM45 and MTM45-1, have been demonstrated to offer mechanical performance and toughness at a level comparable to that of state-of-the-art toughened resin systems used for military and civil airframes, while still permitting cure at relatively low temperatures out of the autoclave. The level of maturity of the new materials, perceived and otherwise, together with the limited amount of available performance data, is currently limiting the application of this much needed technology on aircraft programs. Significant progress has been made to address this situation by embarking on a program of work over the last three years which has put in place the baseline design allowable data and addresses manufacturability issues which arise with non-autoclave curing.
15. SUBJECT TERMS

Autoclave, resins, oven vacuum bag cure (OVBC)
16. SECURITY CLASSIFICATION OF: a. REPORT b. ABSTRACT c. THIS PAGE 18. NUMBER 17. LIMITATION OF PAGES OF ABSTRACT: 19a. NAME OF RESPONSIBLE PERSON (Monitor)

Unclassified Unclassified

Unclassified

SAR

86

Tara Storage
19b. TELEPHONE NUMBER (Include Area Code)

(937) 255-9018
Standard Form 298 (Rev. 8-98) Prescribed by ANSI Std. Z39-18

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Summary After several years of effort funded by the Advanced Composites Group, Inc. (ACG) Internal Research and Development (IRAD) expenditure, a new generation of out of autoclave processable resin systems has been developed which it is believed will replace older oven vacuum bag cure (OVBC) resins such as ACG’s LTM45EL material. The first of these new resins, MTM45 and MTM45-1, have been demonstrated to offer mechanical performance and toughness at a level comparable to that of state-of the-art toughened resin systems used for military and civil airframes, while still permitting cure at relatively low temperatures out of the autoclave. The latter characteristic is important for prototype programs where low-cost tooling is highly desirable given the small number of parts over which tooling costs can be amortized. Once a program transitions into production, the issues are different and include the costs of ownership and operation of tools, springback, molding accuracy and associated assembly costs. MTM45 and MTM45-1 are designed as variable cure cycle materials with initial cures in the range 175°F to 350°F. It is believed that the new generation of materials, of which MTM45 is the first, provides the ability of transitioning from prototyping to production without a change of material and offering significant cost reductions in both circumstances. The basic characteristics of the new out-of-autoclave (OOA) ACG materials are summarized as follows: Table 1. ACG Next Generation Out-of-Autoclave Systems
Resin MTM45 MTM45-1 Form OVBC capability Wet Service >250°F (>121°C) >250°F (>121°C) >250°F (>121°C) >250°F (>121°C) >220°F (>104°C) >180°F (>82°C) Comments Suitable for both prototype and production Higher viscosity variant of MTM45. Further toughness improvement over MTM45 Under evaluation at AFRL

Prepreg, 180°F – 350°F Cure 21 day out life (82°C – 177°C) Cure

Prepreg + RFI 180°F – 350°F Cure (82°C – 177°C) Cure film, 21 day out life 270°F – 350°F Cure MTM44-1 Prepreg and (132°C – 177°C) Cure RFI film, 21 day out life MVR444 VARTM resin, 180°F(82°C) infusion Pot life 5 hours 200°F – 270°F Cure (93°C – 132°C Cure) at 180°F 180°F – 270°F Cure MTM46 Prepreg, >60 day out (82°C – 132°C Cure) life 150°F – 270°F Cure VTM243FRB, Prepreg, VTM244FRB fire retardant (65°C – 132°C Cure) 21 day out life

Lower cost than MTM45, MTM45-1, Lower toughness Lower cost than MTM45, MTM45-1, Lower toughness

The level of maturity of the new materials, perceived and otherwise, together with the limited amount of available performance data, is currently limiting the application of this much needed technology on aircraft programs. Significant progress has been made to address this situation by embarking on a program of work over the last three years which has put in place the baseline design allowable data and addresses the numerous manufacturability issues which arise with non-autoclave curing. A previous Air Force

1

funded contract, F42620-00-D-0039, RZ14, entitled “Low Temperature Composite Processing MTM45 and MTM45-1 Prepregs” and the current contract, FA8650-05-D5807, TO00019, entitled “Complex Structures for Manned/Unmanned Aerial Vehicles” developed the processing techniques and B basis coupon level data up to laminate level on several product forms as shown in the following table and in the subsequent Excel spreadsheets. Data includes static lamina, static laminate unnotched tension and compression, static laminate open and filled hole tension, static laminate open and filled hole compression, laminate bearing, interlaminar, and durability and damage tolerance testing at subambient, ambient, elevated dry, and elevated wet conditions. The alternate cure cycles were designated “LH,” “M,” and “MH” where the LH consisted of a 180°F cure followed by a 350°F postcure, M consisted of a 250°F cure and no postcure, and MH consisted of a 250°F cure and a 350°F postcure.

Table 2. MTM45 and MTM45-1 Allowables Databases Resin MTM45-1 MTM45-1 MTM45-1 MTM45-1 MTM45-1 MTM45 MTM45 Fiber-Aerial Wt.-Resin Wt. 12K AS4-145gsm-32% 3K CF0525 (AS4)-193gsm-36% 12K IM7-145gsm-32% 4581-288gsm-35% GF0103 (7781)-303gsm -35% 6K CF2412 (AS4C)-375gsm-36% 12K AS4C-145gsm-32% Fiber Type Unidirectional Carbon Plain Weave Carbon Fabric Unidirectional Carbon 8HS Astroquartz III Fabric 8HS E-glass Fabric 5HS Carbon Fabric Unidirectional Carbon Cure LH, M, MH LH, M, MH LH, M, MH MH MH LH, M, MH LH, M, MH

The data generated under the current subcontract and contained in the separate spreadsheets were based specifically on the MTM45-1 IM7 unidirectional material and form part of this final report. The statistical analysis work on these and the other data sets is being carried out by the National Center for Advanced Material Performance (NCAMP). The databases have been be generated in accordance with FAA approval procedures and are therefore be usable for commercial aircraft programs as well as military.

2

Material: MTM45/CF2412-36%RW
Test Type: Test Method: Condition: Date of Test: Specimen ID AITR1392-5HC-WT-E-M1-CTD-1 AITR1392-5HC-WT-E-M1-CTD-2 AITR1392-5HC-WT-E-M1-CTD-3 AITR1392-5HC-WT-E-M1-CTD-4 AITR1392-5HC-WT-E-M2-CTD-1 AITR1392-5HC-WT-E-M2-CTD-2 AITR1392-5HC-WT-E-M2-CTD-3 AITR1392-5HC-WT-E-M2-CTD-4 Warp Tensile ASTM D3039/D3039 CTD 2/18/05

Normalization: Cured Ply Thickness: 0.0153 # Plies: 8 Test Report #_____________ Laboratory Ambient:___69____°F, ___30____%RH Table#___________________ Soak @ Test Environment:___5-6_____Minutes Raw Data, Tabular Report Date In:__N/A______ Out:___N/A_____ Laminate Mechanical Testing Modulus/Poisson's Range:_0.1% - 0.3%__ Alignment %:__<5.0%____ Width, Thickness, Cured Ply Ultimate Failure Ultimate Strength, ksi Poisson’s Modulus, Msi Length, in. Measured Normalized Measured Normalized in. in. Thickness: Load, lb. Mode Ratio 10.004 1.0028 0.1205 0.0151 17665 XVV 146.188 143.919 9.23 9.09 Not Tested Not Tested 10.004 1.0040 0.1223 0.0153 16712 XVV 136.103 135.992 9.09 9.08 Not Tested 10.003 1.0014 0.1242 0.0155 17886 ZVV 143.808 145.923 8.81 8.94 Not Tested 10.003 1.0031 0.1246 0.0156 17497 XVV 139.991 142.508 8.67 8.82 Not Tested 10.001 1.0036 0.1201 0.0150 17566 XVV 145.737 142.998 9.36 9.18 Not Tested 10.001 1.0036 0.1225 0.0153 17351 XVV 141.133 141.248 9.08 9.09 Not Tested 10.001 1.0034 0.1239 0.0155 16626 XGM 133.734 135.373 8.65 8.75 Not Tested 10.001 1.0032 0.1251 0.0156 16204 XVV 129.115 131.963 8.82 9.01

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens

10.001 10.004 10.002 0.0014 0.01 8

1.0014 1.0040 1.0031 0.0008 0.08 8

0.1201 0.1251 0.1229 0.0019 1.52 8

0.0150 0.0156 0.0154 0.0002 1.52 8

16204 17886 17188 596 3.47 8

129.115 146.188 139.476 6.068 4.35 8

131.963 145.923 139.991 4.918 3.51 8

8.65 9.36 8.96 0.26 2.95 8

8.75 9.18 9.00 0.15 1.63 8

Tested By:______________________________________ Date:_____________ Notes:

2/29/2008

3

Material: MTM45/CF2412-36%RW
Test Type: Test Method: Condition: Date of Test: Specimen ID AITR1392-5HC-WT-B-LH1-CTD-1 AITR1392-5HC-WT-B-LH1-CTD-2 AITR1392-5HC-WT-B-LH1-CTD-3 AITR1392-5HC-WT-B-LH2-CTD-1 AITR1392-5HC-WT-B-LH2-CTD-2 AITR1392-5HC-WT-B-LH2-CTD-3 AITR1392-5HC-WT-F-LH3-CTD-1 AITR1392-5HC-WT-F-LH3-CTD-2 AITR1392-5HC-WT-F-LH3-CTD-3 Warp Tensile ASTM D3039/D3039 CTD 2/17/05

Normalization: Cured Ply Thickness: 0.0153 Laboratory Ambient:___69____°F, ___31____%RH Soak @ Test Environment:___5-6_____Minutes

# Plies:

8

Test Report #_____________ Table#___________________ Raw Data, Tabular Report Laminate Mechanical Testing
Poisson’s Ratio Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested

Modulus/Poisson's Range:_0.1% - 0.3%__ Width, Thickness, Cured Ply Ultimate Length, in. in. in. Thickness: Load, lb. 10.004 0.9989 0.1232 0.0154 13612 10.004 0.9994 0.1255 0.0157 15039 10.004 0.9990 0.1266 0.0158 16030 10.003 0.9992 0.1230 0.0154 16720 10.003 0.9997 0.1260 0.0158 16559 10.003 0.9990 0.1268 0.0159 17151 10.000 1.0037 0.1152 0.0144 15812 9.999 1.0022 0.1167 0.0146 15106 10.001 1.0044 0.1176 0.0147 16157

Failure Mode LAV LAT LGT LAT LAT LAV LVV LGV LGV

Ultimate Strength, ksi Modulus, Msi Measured Normalized Measured Normalized 110.609 111.332 9.48 9.54 119.905 122.941 9.44 9.67 126.746 131.095 9.37 9.69 136.044 136.711 9.31 9.36 131.460 135.327 9.14 9.41 135.396 140.263 9.46 9.80 136.751 128.707 8.67 8.16 129.159 123.144 8.50 8.11 136.788 131.423 9.54 9.16

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens

9.999 10.0035 10.002 0.0017 0.0171 9

0.9989 1.0044 1.0006 0.0022 0.22 9

0.1152 0.1268 0.1223 0.0046 3.75 9

0.0144 0.0159 0.0153 0.0006 3.75 9

13612 17151 15798 1077 6.82 9

110.609 136.788 129.206 8.965 6.94 9

111.332 140.263 128.994 8.802 6.82 9

8.50 9.54 9.21 0.37 4.06 9

8.11 9.80 9.21 0.64 6.95 9

Tested By:______________________________________ Date:_____________ Notes:

WT-CTD

4

LT-CTD

Longitudinal Tension Properties (LT) -- (CTD) Strength & Modulus
MTM45/ AS4C 12K Unidirectional Prepreg Specimen Number CCJA111B CCJA112B CCJA113B CCJA114B CCJA211B CCJA212B CCJA213B CCJB111B CCJB112B CCJB113B CCJB114B CCJB211B CCJB212B CCJB213B CCJB214B CCJD111B CCJD112B CCJD216B CCJD217B CCJD218B ACG Batch # A A A A A A A B B B B B B B B D D D D D ACG Cure Cycle MH1 MH1 MH1 MH1 MH2 MH2 MH2 MH1 MH1 MH1 MH1 MH2 MH2 MH2 MH2 MH1 MH1 MH2 MH2 MH2 Prepreg Lot # 1 1 1 1 1 1 1 2 2 2 2 2 2 2 2 3 3 3 3 3 Cure Cycle Batch # 1 1 1 1 2 2 2 3 3 3 3 4 4 4 4 5 5 6 6 6 Strength [ksi] 259.076 259.223 281.464 270.912 263.951 268.854 295.626 302.462 269.126 267.301 273.679 281.945 275.321 271.005 252.030 291.500 308.311 303.202 306.057 285.133 Modulus [Msi] 18.886 17.145 18.818 17.363 19.319 18.615 17.885 18.637 17.828 18.872 19.331 19.071 18.130 18.505 18.129 18.161 17.779 17.735 17.979 18.326 0.635 3.464 17.145 19.331 19 Poisson's Ratio 0.343 0.305 0.316 0.314 0.307 0.301 0.307 0.301 0.293 0.310 0.310 0.323 0.304 0.311 0.422 0.283 0.326 0.301 0.281 0.314 0.030 9.532 0.281 0.422 19 Avg. Specimen Thickn. [in] 0.090 0.090 0.090 0.090 0.084 0.087 0.089 0.093 0.093 0.093 0.093 0.087 0.087 0.087 0.087 0.090 0.092 0.093 0.092 0.093 # Plies in Laminate 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 16 Failure Mode SGM SGM SGM SGM SGM SGM SGM XGM/SGM XGM/SGM XGM/SGM XGM/SGM XGM/SGM XGM/SGM XGM/SGM XGM/SGM XGM,SGM XGM,SGM XGM, SGM XGM, SGM XGM, SGM Avg. tply [in] 0.0056 0.0056 0.0056 0.0056 0.0052 0.0054 0.0055 0.0058 0.0058 0.0058 0.0058 0.0054 0.0054 0.0054 0.0054 0.0056 0.0057 0.0058 0.0057 0.0058 0.0056

normalizing tply [in] 0.0055 Strengthnorm [ksi] 264.129 264.721 288.180 276.300 250.753 266.003 297.753 319.647 283.806 282.843 289.229 278.848 271.880 267.412 248.498 298.125 320.807 319.626 319.274 302.414 285.512 22.747 7.967 248.498 320.807 20 Modulusnorm [Msi] 19.255 17.509 19.192 16.494 19.114 18.749 18.901 19.654 18.865 19.944 19.118 18.833 17.889 18.246 18.541 18.897 18.742 18.501 19.069 18.711 0.776 4.145 16.494 19.944 19

Average 279.309 Standard Dev. 16.954 Coeff. of Var. [%] 6.070 Min. 252.030 Max. 308.311 Number of Spec. 20

Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

0.0052 0.0058

Prepared by NIAR COMPOSITES LABORATORY 2/29/2008

5

Material: MTM45/AS4C-145-32%RW
Test Type: Test Method: Condition: Date of Test: Specimen ID AITR1392-ASU-LT-J-M1-CTD-1 AITR1392-ASU-LT-J-M1-CTD-2 AITR1392-ASU-LT-J-M1-CTD-3 AITR1392-ASU-LT-J-M1-CTD-4 AITR1392-ASU-LT-J-M2-CTD-1 AITR1392-ASU-LT-J-M2-CTD-2 AITR1392-ASU-LT-J-M2-CTD-3 AITR1392-ASU-LT-J-M2-CTD-4 Longitudinal Tensile ASTM D3039/D3039 CTD 2/21/05

Normalization: Cured Ply Thickness: 0.0055 # Plies: 16 Test Report #_____________ Laboratory Ambient:___70____°F, ___39____%RH Table#___________________ Soak @ Test Environment:___5-6_____Minutes Raw Data, Tabular Report Date In:__N/A______ Out:___N/A_____ Laminate Mechanical Testing Modulus/Poisson's Range:_0.1% - 0.3%__ Alignment %:__<5.0%____ Poisson’s Width, Thickness, Cured Ply Ultimate Failure Ultimate Strength (1), ksi Modulus, Msi Length, in. Measured Normalized Measured Normalized Ratio in. in. Thickness: Load, lb. Mode 10.029 0.9970 0.0900 0.0056 N/A N/A 308.316 298.747 18.18 18.60 Not Tested 10.033 0.9969 0.0904 0.0057 N/A N/A 335.020 324.622 18.22 18.72 Not Tested 10.027 0.9979 0.0811 0.0051 N/A N/A 308.316 298.747 17.58 16.21 Not Tested 10.028 0.9967 0.0866 0.0054 N/A N/A 297.228 288.003 18.28 17.99 Not Tested 10.034 0.9960 0.0785 0.0049 N/A N/A 254.981 247.067 18.15 16.19 Not Tested 10.031 0.9955 0.0841 0.0053 N/A N/A 304.161 294.721 18.55 17.73 Not Tested 10.032 0.9955 0.0878 0.0055 N/A N/A 316.824 306.990 18.57 18.52 Not Tested 10.030 0.9965 0.0888 0.0056 N/A N/A 297.546 288.311 18.52 18.69 Not Tested

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens

10.027 10.034 10.031 0.002 0.02 8

0.9955 0.9979 0.9965 0.0008 0.08 8

0.0785 0.0904 0.0859 0.0043 5.03 8

0.0049 0.0057 0.0054 0.0003 5.03 8

254.98 335.02 302.80 22.81 7.53 8.00

247.07 324.62 293.40 22.10 7.53 8.00

17.58 18.57 18.26 0.32 1.76 8

16.19 18.72 17.83 1.07 5.97 8

Tested By:______________________________________ Date:_____________ Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable (1) Derived in accordance with AI/TR/1392 Table 3a , note (1)

LT-CTD

6

Material: MTM45/AS4C-145-32%RW
Test Type: Test Method: Condition: Date of Test: Specimen ID AITR1392-ASU-LT-J-LH1-CTD-1 AITR1392-ASU-LT-J-LH1-CTD-2 AITR1392-ASU-LT-J-LH1-CTD-3 AITR1392-ASU-LT-J-LH2-CTD-1 AITR1392-ASU-LT-J-LH2-CTD-2 AITR1392-ASU-LT-J-LH2-CTD-3 AITR1392-ASU-LT-J-LH3-CTD-1 AITR1392-ASU-LT-J-LH3-CTD-2 AITR1392-ASU-LT-J-LH3-CTD-3 Longitudinal Tensile ASTM D3039/D3039 CTD 2/21/05

Normalization: Cured Ply Thickness: 0.0055 # Plies: 16 Test Report #_____________ Laboratory Ambient:___70____°F, ___39____%RH Table#___________________ Soak @ Test Environment:___5-6_____Minutes Raw Data, Tabular Report Date In:__N/A______ Out:___N/A_____ Laminate Mechanical Testing Modulus/Poisson's Range:_0.1% - 0.3%__ Width, Thickness, Cured Ply Ultimate Failure Ultimate Strength (1), ksi Poisson’s Modulus, Msi Length, in. Measured Normalized Measured Normalized in. in. Thickness: Load, lb. Mode Ratio 10.033 0.9979 0.0880 0.0055 N/A N/A 323.333 306.758 18.86 18.86 Not Tested N/A N/A 305.094 289.454 18.97 18.21 Not Tested 10.032 0.9985 0.0845 0.0053 N/A N/A 298.612 283.305 18.40 18.30 Not Tested 10.028 0.9978 0.0875 0.0055 N/A N/A 306.613 290.896 18.90 17.70 Not Tested 10.030 0.9974 0.0824 0.0052 N/A N/A 316.035 299.834 18.90 16.11 Not Tested 10.027 0.9971 0.0750 0.0047 N/A N/A 301.749 286.280 18.69 18.29 Not Tested 10.031 0.9975 0.0861 0.0054 N/A N/A 331.191 314.213 20.09 17.97 Not Tested 10.043 1.0028 0.0787 0.0049 N/A N/A 335.828 318.613 19.62 19.06 Not Tested 10.046 1.0033 0.0855 0.0053 N/A N/A 331.692 314.689 21.46 18.46 Not Tested 10.047 1.0029 0.0757 0.0047

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens

10.027 10.047 10.0352 0.008 0.08 9

0.9971 1.0033 0.9995 0.0027 0.27 9

0.0750 0.0880 0.0826 0.0050 6.02 9

0.0047 0.0055 0.0052 0.0003 6.02 9

298.61 335.83 316.68 14.28 4.51 9

283.30 318.61 300.45 13.55 4.51 9

18.40 21.46 19.32 0.95 4.90 9

16.11 19.06 18.11 0.86 4.73 9

Tested By:______________________________________ Date:_____________ Notes: (1) Derived in accordance with AI/TR/1392 Table 3a , note (1)

2/29/2008

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LT-CTD

DATA REDUCTION TABLE FOR ASTM D3039 TENSILE PROPERTIES OF POLYMER MATRIX COMPOSITE MATERIALS (STRENGTH AND MODULUS)

BATCH NAME: AFJA X1XB ACG CODE AFJA 11XB SPECIMEN # IMU-LT-A-MH1-CTD-1 IMU-LT-A-MH1-CTD-2 IMU-LT-A-MH1-CTD-3 IMU-LT-A-MH1-CTD-4 AFJA 21XB IMU-LT-A-MH2-CTD-1 IMU-LT-A-MH2-CTD-2 IMU-LT-A-MH2-CTD-3 IMU-LT-A-MH2-CTD-4 CURE CYCLE 1 1 1 1 2 2 2 2 AVG WIDTH [in] 1.006 1.006 1.006 1.005 1.007 1.008 1.007 1.008

CONDITION (CTD, ETD, ETW) : CTD AVG THICK [in] 0.089 0.092 0.091 0.091 0.086 0.085 0.086 0.086 INITIAL LOAD OFFSET [lb] 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 MAX LOAD [lb] 26919.2 26328.5 22871.9 21203.7 TENSILE STRENGTH [ksi] 299.225 284.529 249.940 232.569 TENSILE MODULUS [Msi] 21.617 22.357 22.023 22.158 FINAL STRAIN [microstrain] 9968.022 13579.954 12839.110 13362.464 STRAIN RANGE [microstrain] 1000-3000 1000-3000 1000-3000 1000-3000 TEST TEMP [o F] -65 F -65 F -65 F -65 F COMMENTS/ FAILURE MODE SGM SGM SGM SGM

AFJB 11XB

IMU-LT-B-MH1-CTD-1 IMU-LT-B-MH1-CTD-2 IMU-LT-B-MH1-CTD-3 IMU-LT-B-MH1-CTD-4

1 1 1 1 2 2 2 2

1.006 1.007 1.007 1.007 1.000 1.008 1.009 1.008

0.097 0.096 0.097 0.095 0.093 0.097 0.096 0.095

0.0 0.0 0.0

33141.5 31437.0 27876.5

341.421 324.004 286.388

21.962 22.616 22.548

14104.844 14310.692 13994.201

1000-3000 1000-3000 1000-3000

-65 F -65 F -65 F

XGM XGM XGM

AFJB 21XB

IMU-LT-B-MH2-CTD-1 IMU-LT-B-MH2-CTD-2 IMU-LT-B-MH2-CTD-3 IMU-LT-B-MH2-CTD-4

0.0 0.0 0.0 0.0

29181.548 32009.759 35823.573 33333.229

312.896 325.937 370.017 349.056

21.220 22.691 22.933 22.992

13591.946 14634.534 14258.172 12853.440

1000-3000 1000-3000 1000-3000 1000-3000

-65 F -65 F -65 F -65 F

XGM XGM XGM XGM

AFJC 11XB

IMU-LT-C-MH1-CTD-1 IMU-LT-C-MH1-CTD-2 IMU-LT-C-MH1-CTD-3 IMU-LT-C-MH1-CTD-4

1 1 1 1 2 2 2 2

1.007 1.007 1.007 1.007 1.009 1.009 1.009 1.009

0.087 0.088 0.088 0.088 0.088 0.088 0.089 0.089 0.0 0.0 0.0 30618.665 28226.156 29410.577 344.088 313.232 328.039 22.582 21.837 22.659 14144.664 13101.648 14645.665 1000-3000 1000-3000 1000-3000 -65 F -65 F -65 F XGM XGM XGM 0.0 0.0 0.0 26921.5 22565.1 30617.2 304.175 254.904 343.873 22.182 22.953 22.367 14167.631 12696.878 13605.343 1000-3000 1000-3000 1000-3000 -65 F -65 F -65 F XGM XGM XGM

AFJC 21XB

IMU-LT-C-MH2-CTD-1 IMU-LT-C-MH2-CTD-2 IMU-LT-C-MH2-CTD-3 IMU-LT-C-MH2-CTD-4

LOAD FRAME CAPACITY LOAD CELL EXTENSOMETER MODEL STR.GAGE/EXT.MTR I.D GAUGE FACTOR EXCITATION VOLTAGE GAUGE RESISTANCE

55 kips 55000 lbs N/A CEA-06-250UW-350 2.105 5.0 volts 350.0 ohms

AVERAGE TENSILE STRENGTH [ksi] STANDARD DEVIATION [ksi] COEFFICIENT OF VARIATION [%]

309.664 38.088 12.300

AVERAGE TENSILE MODULUS [Msi] STANDARD DEVIATION [Msi] COEFFICIENT OF VARIATION [%]

22.335 0.493 2.207

NAME DIMENSIONING

DATE

Proprietary Data

Prepared by NIAR Center for Advanced Material Performance (CAMP)

2/29/2008

8

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test LT

Cure Cycle Condition M CTD

Test Group: AITR1392-IMU-LT-M-CTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-LT-C-M1-CTD-1 AITR1392-IMU-LT-C-M1-CTD-2 AITR1392-IMU-LT-C-M1-CTD-3 AITR1392-IMU-LT-C-M1-CTD-4 AITR1392-IMU-LT-C-M1-CTD-5 AITR1392-IMU-LT-C-M2-CTD-1 AITR1392-IMU-LT-C-M2-CTD-2 AITR1392-IMU-LT-C-M2-CTD-3 AITR1392-IMU-LT-C-M2-CTD-4 AITR1392-IMU-LT-C-M2-CTD-5 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 CTD Condition: Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Failure Mode Ultimate Strength , ksi Length, in. Width, in. Measured Normalized in. Thickness: Load, lb. NT NT NT NT NT 10.064 1.0096 0.0908 0.0057 NT 365.144 366.182 10.064 1.0016 0.0905 0.0057 NT 10.066 1.0016 0.0908 0.0057 NT 352.336 352.569 10.066 1.0016 0.0903 0.0056 NT 374.514 376.890 10.065 1.0022 0.0903 0.0056 NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized NT NT NT NT NT 22.72 23.44 GE 23.61 24.36 22.35 22.93 22.67 23.27 Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0636 10.0661 10.0649 0.0012 0.01 5

1.0016 1.0096 1.0033 0.0035 0.35 5

0.0903 0.0908 0.0905 0.0002 0.27 5

0.0056 0.0057 0.0057 0.0000 0.27 5

352.336 374.514 363.998 11.133 3.06 3

352.569 376.890 365.214 12.189 3.34 3

22.350 23.606 22.836 0.539 2.36 4

22.934 24.357 23.499 0.609 2.59 4

(1) Derived in accordance with AI/TR/1392 Table 3a , note (1) FORM MP1112 (ASTMD3039) 2/29/2008

9

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test LT

Cure Cycle Condition LH CTD

Test Group: AITR1392-IMU-LT-LH-CTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-LT-C-LH1-CTD-1 AITR1392-IMU-LT-C-LH1-CTD-2 AITR1392-IMU-LT-C-LH1-CTD-3 AITR1392-IMU-LT-C-LH1-CTD-4 AITR1392-IMU-LT-C-LH1-CTD-5 AITR1392-IMU-LT-C-LH2-CTD-1 AITR1392-IMU-LT-C-LH2-CTD-2 AITR1392-IMU-LT-C-LH2-CTD-3 AITR1392-IMU-LT-C-LH2-CTD-4 AITR1392-IMU-LT-C-LH2-CTD-5 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 CTD Condition: Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Length, in. Width, in. Failure Mode Ultimate Strength , ksi Measured Normalized in. Thickness: Load, lb. 10.063 1.0051 0.0879 0.0055 NT 325.124 323.308 10.061 1.0053 0.0847 0.0053 NT 334.889 325.692 10.061 1.0059 0.0868 0.0054 NT 334.800 328.459 10.063 1.0059 0.0872 0.0055 NT 310.890 307.975 10.060 1.0059 0.0876 0.0055 NT NT NT NT NT NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 22.55 22.52 23.07 22.22 22.86 22.55 23.17 22.96 Poisson’s Ratio NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0602 10.0634 10.0617 0.0013 0.01 5

1.0051 1.0059 1.0056 0.0004 0.04 5

0.0847 0.0879 0.0869 0.0013 1.45 5

0.0053 0.0055 0.0054 0.0001 1.45 5

310.890 334.889 326.426 11.326 3.47 4

307.975 328.459 321.358 9.167 2.85 4

22.547 23.173 22.914 0.277 1.21 4

22.217 22.962 22.564 0.306 1.36 4

(1) Derived in accordance with AI/TR/1392 Table 3a , note (1) FORM MP1112 (ASTMD3039) 2/29/2008

10

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test LT

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-LT-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-LT-C-LH1-RTD-1 AITR1392-IMU-LT-C-LH1-RTD-2 AITR1392-IMU-LT-C-LH1-RTD-3 AITR1392-IMU-LT-C-LH1-RTD-4 AITR1392-IMU-LT-C-LH1-RTD-5 AITR1392-IMU-LT-C-LH2-RTD-1 AITR1392-IMU-LT-C-LH2-RTD-2 AITR1392-IMU-LT-C-LH2-RTD-3 AITR1392-IMU-LT-C-LH2-RTD-4 AITR1392-IMU-LT-C-LH2-RTD-5 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 RTD Condition: Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Length, in. Width, in. Failure Mode Ultimate Strength , ksi Measured Normalized in. Thickness: Load, lb. 10.063 1.0057 0.0874 0.0055 NT 339.367 336.154 10.061 1.0054 0.0868 0.0054 NT 346.996 343.348 10.064 1.0061 0.0872 0.0054 NT 327.640 324.817 10.064 1.0060 0.0868 0.0054 NT 341.820 336.770 10.063 1.0059 0.0879 0.0055 NT NT NT NT NT NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 21.14 20.99 22.99 22.68 22.84 22.62 22.59 22.28 Poisson’s Ratio NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0613 10.0638 10.0630 0.0010 0.01 5

1.0054 1.0061 1.0058 0.0003 0.03 5

0.0868 0.0879 0.0872 0.0005 0.52 5

0.0054 0.0055 0.0055 0.0000 0.52 5

327.640 346.996 338.956 8.186 2.42 4

324.817 343.348 335.272 7.693 2.29 4

21.135 22.985 22.387 0.850 3.80 4

20.987 22.680 22.144 0.791 3.57 4

(1) Derived in accordance with AI/TR/1392 Table 3a , note (1) FORM MP1112 (ASTMD3039) 2/29/2008

11

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test LC

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-LC-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-LC-C-LH1-RTD-1 AITR1392-IMU-LC-C-LH1-RTD-2 AITR1392-IMU-LC-C-LH1-RTD-3 AITR1392-IMU-LC-C-LH1-RTD-4 AITR1392-IMU-LC-C-LH1-RTD-5 AITR1392-IMU-LC-C-LH2-RTD-1 AITR1392-IMU-LC-C-LH2-RTD-2 AITR1392-IMU-LC-C-LH2-RTD-3 AITR1392-IMU-LC-C-LH2-RTD-4 AITR1392-IMU-LC-C-LH2-RTD-5 Longitudinal Compression MP1114 (ASTMD6641)

Cured Ply Thickness: 0.0055 #Plies: 16 RTD Condition: Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Length, in. Width, in. Failure Mode Ultimate Strength , ksi Measured Normalized in. Thickness: Load, lb. 5.499 0.5060 0.0888 0.0055 NT 206.803 207.194 5.499 0.5066 0.0903 0.0056 NT 205.032 207.459 5.499 0.5075 0.0897 0.0056 NT 201.415 203.322 5.499 0.5077 0.0888 0.0056 NT 195.344 195.658 5.499 0.5059 0.0882 0.0055 NT 213.131 212.263 NT NT NT NT NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 20.66 20.84 19.49 19.99 20.06 20.44 18.75 18.93 20.93 20.97 Poisson’s Ratio 0.334 0.375 0.342 0.341 0.340

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

5.4986 5.4987 5.4987 0.0001 0.00 5

0.5059 0.5077 0.5067 0.0008 0.16 5

0.0882 0.0903 0.0891 0.0008 0.93 5

0.0055 0.0056 0.0056 0.0001 0.93 5

195.344 213.131 204.345 6.582 3.22 5

195.658 212.263 205.179 6.195 3.02 5

18.754 20.928 19.977 0.883 4.42 5

18.928 20.968 20.234 0.825 4.08 5

0.3340 0.3750 0.3464 0.0163 4.70 5

(1) Derived in accordance with AI/TR/1392 Table 3a , note (1) FORM MP1114 (ASTMD6641) 2/29/2008

12

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test TT

Cure Cycle Condition LH CTD

Test Group: AITR1392-IMU-TT-LH-CTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-TT-C-LH1-CTD-1 AITR1392-IMU-TT-C-LH1-CTD-2 AITR1392-IMU-TT-C-LH1-CTD-3 AITR1392-IMU-TT-C-LH1-CTD-4 AITR1392-IMU-TT-C-LH1-CTD-5 AITR1392-IMU-TT-C-LH2-CTD-1 AITR1392-IMU-TT-C-LH2-CTD-2 AITR1392-IMU-TT-C-LH2-CTD-3 AITR1392-IMU-TT-C-LH2-CTD-4 AITR1392-IMU-TT-C-LH2-CTD-5 Transverse Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.056 1.0042 0.0881 0.0055 430.00 LWB 4.859 4.866 1.23 1.23 10.085 1.0054 0.0880 0.0055 343.00 LAB 3.878 3.884 1.30 1.30 10.057 1.0020 0.0879 0.0055 355.00 LWB 4.030 4.037 1.25 1.25 10.056 1.0015 0.0877 0.0055 393.00 LGM 4.473 4.480 1.07 1.07 10.086 1.0039 0.0883 0.0055 477.00 LGM 5.383 5.391 1.28 1.28 10.070 1.0040 0.0877 0.0055 413.00 LGM 4.691 4.698 1.26 1.26 10.083 1.0051 0.0877 0.0055 408.00 LWT 4.627 4.634 1.24 1.24 10.071 1.0042 0.0874 0.0055 405.00 LAB 4.616 4.623 1.26 1.25 10.074 1.0041 0.0878 0.0055 443.00 LAB 5.023 5.031 1.28 1.27 10.073 1.0050 0.0878 0.0055 NT NT

Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0563 10.0861 10.0712 0.0115 0.11 10

1.0015 1.0054 1.0039 0.0013 0.13 10

0.0874 0.0883 0.0878 0.0002 0.28 10

0.0055 0.0055 0.0055 0.0000 0.28 10

343.00 477.00 407.44 41.47 10.18 9

3.878 5.383 4.620 0.465 10.06 9

3.884 5.391 4.627 0.465 10.06 9

1.072 1.302 1.240 0.067 5.41 9

1.069 1.302 1.238 0.068 5.46 9

FORM MP1112 (ASTMD3039) 2/29/2008

13

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test TT

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-TT-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-TT-C-LH1-RTD-1 AITR1392-IMU-TT-C-LH1-RTD-2 AITR1392-IMU-TT-C-LH1-RTD-3 AITR1392-IMU-TT-C-LH1-RTD-4 AITR1392-IMU-TT-C-LH1-RTD-5 AITR1392-IMU-TT-C-LH2-RTD-1 AITR1392-IMU-TT-C-LH2-RTD-2 AITR1392-IMU-TT-C-LH2-RTD-3 AITR1392-IMU-TT-C-LH2-RTD-4 AITR1392-IMU-TT-C-LH2-RTD-5 Transverse Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process RTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.056 1.0039 0.0878 0.0055 363.00 LGM 4.118 4.109 1.15 1.15 10.086 1.0041 0.0883 0.0055 367.00 LGM 4.138 4.130 1.14 1.15 10.038 1.0035 0.0879 0.0055 FM LIB 1.14 1.14 10.086 1.0034 0.0881 0.0055 401.00 LGM 4.535 4.526 1.16 1.16 10.086 1.0045 0.0886 0.0055 397.00 LGM 4.461 4.452 1.14 1.15 10.081 1.0049 0.0876 0.0055 348.00 LAT 3.953 3.945 1.16 1.15 10.083 1.0051 0.0876 0.0055 348.00 LGM 3.952 3.944 1.16 1.16 10.084 1.0048 0.0875 0.0055 353.00 LGM 4.017 4.009 1.14 1.13 10.084 1.0048 0.0875 0.0055 367.00 LWB 4.173 4.164 1.16 1.15 10.084 1.0051 0.0875 0.0055 318.00 LAT 3.617 3.610 1.15 1.14

Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0377 10.0862 10.0767 0.0164 0.16 10

1.0034 1.0051 1.0044 0.0006 0.06 10

0.0875 0.0886 0.0878 0.0004 0.45 10

0.0055 0.0055 0.0055 0.0000 0.45 10

318.00 401.00 362.44 25.51 7.04 9

3.617 4.535 4.107 0.276 6.72 9

3.610 4.526 4.099 0.275 6.72 9

1.141 1.161 1.150 0.008 0.66 10

1.134 1.157 1.148 0.007 0.62 10

FORM MP1112 (ASTMD3039) 2/29/2008

14

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test TC

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-TC-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-TC-C-LH1-RTD-1 AITR1392-IMU-TC-C-LH1-RTD-2 AITR1392-IMU-TC-C-LH1-RTD-3 AITR1392-IMU-TC-C-LH1-RTD-4 AITR1392-IMU-TC-C-LH1-RTD-5 AITR1392-IMU-TC-C-LH2-RTD-1 AITR1392-IMU-TC-C-LH2-RTD-2 AITR1392-IMU-TC-C-LH2-RTD-3 AITR1392-IMU-TC-C-LH2-RTD-4 AITR1392-IMU-TC-C-LH2-RTD-5 Transverse Compression MP1114 (ASTMD6641)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process RTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 5.498 0.5039 0.0884 0.0055 1124.00 HGB/HGT 25.246 25.346 1.27 1.27 5.499 0.5015 0.0888 0.0055 1119.00 HGT 25.137 25.237 1.27 1.28 5.500 0.5024 0.0891 0.0056 1157.00 BGB/HGT 25.850 25.953 1.29 1.30 5.499 0.5042 0.0886 0.0055 1127.00 BGT 25.230 25.330 1.30 1.31 5.499 0.5050 0.0889 0.0056 NT NT 5.502 0.5037 0.0889 0.0056 1109.00 HGB/LAB 24.758 24.857 1.15 1.16 5.503 0.5039 0.0879 0.0055 1000.00 BGM 22.586 22.675 1.25 1.25 5.502 0.5028 0.0892 0.0056 1039.00 BGM 23.169 23.261 1.14 1.15 5.501 0.5041 0.0884 0.0055 1060.00 BGT 23.781 23.875 1.24 1.25 5.502 0.5033 0.0881 0.0055 NT NT

Poisson’s Ratio 0.011 0.012 0.014 0.012 NT GE GE GE 0.011 NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

5.4982 5.5026 5.5006 0.0017 0.03 10

0.5015 0.5050 0.5035 0.0010 0.20 10

0.0879 0.0892 0.0886 0.0004 0.50 10

0.0055 0.0056 0.0055 0.0000 0.50 10

1000.00 1157.00 1091.88 53.17 4.87 8

22.586 25.850 24.470 1.154 4.72 8

22.675 25.953 24.567 1.159 4.72 8

1.136 1.304 1.238 0.062 5.00 8

1.151 1.313 1.247 0.060 4.84 8

0.0110 0.0140 0.0120 0.0012 10.21 5

FORM MP1114 (ASTMD6641) 2/29/2008

15

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test UNT0

Cure Cycle Condition LH CTD

Test Group: AITR1392-IMU-UNT0-LH-CTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-UNT0-C-LH1-CTD-1 AITR1392-IMU-UNT0-C-LH1-CTD-2 AITR1392-IMU-UNT0-C-LH1-CTD-3 AITR1392-IMU-UNT0-C-LH1-CTD-4 AITR1392-IMU-UNT0-C-LH1-CTD-5 AITR1392-IMU-UNT0-C-LH2-CTD-1 AITR1392-IMU-UNT0-C-LH2-CTD-2 AITR1392-IMU-UNT0-C-LH2-CTD-3 AITR1392-IMU-UNT0-C-LH2-CTD-4 AITR1392-IMU-UNT0-C-LH2-CTD-5 0/90 Unnotched Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.083 1.0050 0.0871 0.0054 15584.00 LWB/LAT 177.991 176.204 12.52 12.40 10.081 1.0049 0.0864 0.0054 15924.00 LAB/LAT 183.336 181.496 12.43 12.21 10.068 1.0051 0.0859 0.0054 15816.00 DGM/LAB/LAT 183.287 181.448 12.36 12.06 10.079 1.0044 0.0872 0.0054 14898.00 LWT/LAB 170.198 168.489 12.32 12.20 10.078 1.0047 0.0876 0.0055 NT NT 10.075 1.0022 0.0869 0.0054 FM LIT 12.53 12.37 10.074 1.0018 0.0868 0.0054 16337.00 LWB/LAT 187.942 186.055 12.94 12.76 10.074 1.0024 0.0867 0.0054 15797.00 DGM/LAT/LAB 181.796 179.971 12.60 12.41 10.073 1.0024 0.0865 0.0054 16091.00 DGM/LAT/LAB 185.506 183.644 12.67 12.46 10.074 1.0019 0.0873 0.0055 16092.00 DGM/LAT/LAB 184.015 182.168 12.52 12.42

Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0677 10.0829 10.0759 0.0045 0.05 10

1.0018 1.0051 1.0035 0.0014 0.14 10

0.0859 0.0876 0.0868 0.0005 0.56 10

0.0054 0.0055 0.0054 0.0000 0.56 10

14898.00 16337.00 15817.38 436.18 2.76 8

170.198 187.942 181.759 5.478 3.01 8

168.489 186.055 179.934 5.423 3.01 8

12.323 12.940 12.544 0.184 1.47 9

12.062 12.759 12.365 0.198 1.60 9

FORM MP1112 (ASTMD3039) 2/29/2008

16

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test UNT0

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-UNT0-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-UNT0-C-LH1-RTD-1 AITR1392-IMU-UNT0-C-LH1-RTD-2 AITR1392-IMU-UNT0-C-LH1-RTD-3 AITR1392-IMU-UNT0-C-LH1-RTD-4 AITR1392-IMU-UNT0-C-LH1-RTD-5 AITR1392-IMU-UNT0-C-LH2-RTD-1 AITR1392-IMU-UNT0-C-LH2-RTD-2 AITR1392-IMU-UNT0-C-LH2-RTD-3 AITR1392-IMU-UNT0-C-LH2-RTD-4 AITR1392-IMU-UNT0-C-LH2-RTD-5 0/90 Unnotched Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process RTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.080 1.0046 0.0870 0.0054 16316.00 LAT/LAB 186.789 184.560 11.93 11.79 188.709 12.46 12.36 10.067 1.0045 0.0873 0.0055 16752.00 LGB/DWB/LAT 190.988 10.068 1.0051 0.0873 0.0055 15824.00 DGB/LAT 180.334 178.183 12.31 12.22 185.894 12.11 11.91 10.069 1.0036 0.0866 0.0054 16352.00 DGB/DAB/LAT 188.139 10.068 1.0042 0.0874 0.0055 NT NT 10.074 1.0020 0.0865 0.0054 16226.00 LWB/LAT/DGB 187.137 184.904 12.56 12.35 10.074 1.0019 0.0864 0.0054 16274.00 LGM/LAT/LAB 187.999 185.756 12.42 12.19 197.099 12.47 12.31 10.076 1.0019 0.0869 0.0054 17371.00 LGM/DWB/LAT 199.479 10.075 1.0030 0.0869 0.0054 15738.00 LGM/LAB/LAT 180.638 178.483 12.32 12.16 10.075 1.0032 0.0875 0.0055 NT NT

Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0672 10.0795 10.0725 0.0041 0.04 10

1.0019 1.0051 1.0034 0.0012 0.12 10

0.0864 0.0875 0.0870 0.0004 0.45 10

0.0054 0.0055 0.0054 0.0000 0.45 10

15738.00 17371.00 16356.63 517.86 3.17 8

180.334 199.479 187.688 6.037 3.22 8

178.183 197.099 185.448 5.965 3.22 8

11.929 12.563 12.322 0.210 1.71 8

11.787 12.364 12.162 0.210 1.72 8

FORM MP1112 (ASTMD3039) 2/29/2008

17

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test UNC0

Cure Cycle Condition LH RTD

Test Group: AITR1392-IMU-UNC0-LH-RTD MTM45-1/IM7-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-IMU-UNC0-C-LH1-RTD-1 AITR1392-IMU-UNC0-C-LH1-RTD-2 AITR1392-IMU-UNC0-C-LH1-RTD-3 AITR1392-IMU-UNC0-C-LH1-RTD-4 AITR1392-IMU-UNC0-C-LH1-RTD-5 AITR1392-IMU-UNC0-C-LH2-RTD-1 AITR1392-IMU-UNC0-C-LH2-RTD-2 AITR1392-IMU-UNC0-C-LH2-RTD-3 AITR1392-IMU-UNC0-C-LH2-RTD-4 AITR1392-IMU-UNC0-C-LH2-RTD-5 90/0 Compression MP1114 (ASTMD6641)

Cured Ply Thickness: 0.0055 #Plies: 16 ACG, Inc. Condition: Material & Process RTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 5.499 0.5034 0.0876 0.0055 4793.00 HIT/BGT 108.752 108.196 10.87 10.81 5.500 0.5042 0.0878 0.0055 4774.00 HIT/BGT 107.821 107.269 10.66 10.64 5.501 0.5042 0.0880 0.0055 4699.00 BGT 105.919 105.377 10.56 10.56 5.501 0.5045 0.0875 0.0055 4533.00 HIB/BGB 102.726 102.201 10.23 10.16 5.501 0.5043 0.0871 0.0054 4924.00 HGT 112.080 111.507 10.21 10.11 NT NT NT NT NT NT NT NT NT NT

Poisson’s Ratio 0.028 0.036 0.021 0.017 0.015 NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

5.4987 5.5014 5.5002 0.0011 0.02 5

0.5034 0.5045 0.5041 0.0004 0.08 5

0.0871 0.0880 0.0876 0.0003 0.38 5

0.0054 0.0055 0.0055 0.0000 0.38 5

4533.00 4924.00 4744.60 143.39 3.02 5

102.726 112.080 107.460 3.461 3.22 5

102.201 111.507 106.910 3.444 3.22 5

10.212 10.869 10.506 0.284 2.71 5

10.109 10.813 10.457 0.307 2.94 5

0.0150 0.0360 0.0234 0.0086 36.84 5

FORM MP1114 (ASTMD6641) 2/29/2008

18

Input:

Test Plan Prefix AITR

Test Plan # 1392

Material IMU

Test IPS

Cure Cycle LH

Condition RTD

Test Group: AITR1392-IMU-IPS-LH-RTD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-IPS-C-LH1-RTD-1 AITR1392-IMU-IPS-C-LH1-RTD-2 AITR1392-IMU-IPS-C-LH1-RTD-3 AITR1392-IMU-IPS-C-LH1-RTD-4 AITR1392-IMU-IPS-C-LH1-RTD-5 AITR1392-IMU-IPS-C-LH2-RTD-1 AITR1392-IMU-IPS-C-LH2-RTD-2 AITR1392-IMU-IPS-C-LH2-RTD-3 AITR1392-IMU-IPS-C-LH2-RTD-4 AITR1392-IMU-IPS-C-LH2-RTD-5 ±45° In Plane Shear MP1115 (ASTMD3518) Length, in. 10.079 10.079 10.079 10.079 10.067 10.067 10.067 10.067 10.065 10.075

Normalization: NA Condition: RTD Modulus/Poisson's Range: Width, in. 1.0031 1.0036 1.0040 1.0031 1.0054 1.0087 1.0091 1.0089 1.0084 1.0088

Cured Ply Thickness: 0.0055 ACG, Inc. #Plies: 8 Material & Process Chord 0.2% to 0.6% Laboratory Report Cured Ply Shear Strength, ksi Failure Mode Thickness, in. Maximum Thickness: 0.2% Offset @ 5% Strain 5.908 0.0451 0.0056 8.820 NT 6.019 0.0447 0.0056 8.840 NT 6.268 0.0450 0.0056 8.760 NT 6.064 NT 0.0444 0.0055 NA 6.296 0.0452 0.0056 8.680 NT 6.470 0.0445 0.0056 9.590 NT 6.312 0.0459 0.0057 9.370 NT 6.567 0.0448 0.0056 9.650 NT 6.560 0.0446 0.0056 9.650 NT 6.560 0.0455 0.0057 9.650 NT

Modulus, Msi Measured NT NT NT NT NT NT NT NT NT NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result NA=Not Applicable FM=Failure Mode Unacceptable GE=Gage Error

10.0646 10.0795 10.0724 0.0064 0.06 10

1.0031 1.0091 1.0063 0.0027 0.27 10

0.0444 0.0459 0.0450 0.0005 1.06 10

0.0055 0.0057 0.0056 0.0001 1.06 10

5.908 6.567 6.302 0.241 3.83 10

8.680 9.650 9.223 0.436 4.73 9

FORM MP1115 (ASTMD3518) 2/29/2008

19

Input:

Test Plan Prefix AITR

Test Plan # 1392

Material IMU

Test SBS

Cure Cycle LH

Condition CTD 0.0055 16 Ultimate Load, lb. 569.00 580.00 554.00 566.00 612.00 NT NT NT NT NT

Test Group: AITR1392-IMU-SBS-LH-CTD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-SBS-C-LH1-CTD-1 AITR1392-IMU-SBS-C-LH1-CTD-2 AITR1392-IMU-SBS-C-LH1-CTD-3 AITR1392-IMU-SBS-C-LH1-CTD-4 AITR1392-IMU-SBS-C-LH1-CTD-5 AITR1392-IMU-SBS-C-LH2-CTD-1 AITR1392-IMU-SBS-C-LH2-CTD-2 AITR1392-IMU-SBS-C-LH2-CTD-3 AITR1392-IMU-SBS-C-LH2-CTD-4 AITR1392-IMU-SBS-C-LH2-CTD-5 Short Beam Shear MP1116 (ASTMD2344) Length, in. 0.559 0.561 0.560 0.561 0.560

Normalization: Cured Ply Thickness: Condition: CTD #Plies: Span (4t): 0.35 Cured Ply Width, in. Thickness, in. Thickness: 0.2530 0.0896 0.0056 0.2500 0.0882 0.0055 0.2525 0.0887 0.0055 0.2515 0.0883 0.0055 0.2545 0.0882 0.0055

ACG, Inc. Material & Process Laboratory Report
Failure Mode ILS ILS ILS ILS ILS Ultimate Strength, ksi Measured Normalized 18.832 19.168 19.728 19.773 18.559 18.699 19.122 19.180 20.441 20.495

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result FM=Failure Mode Unacceptable

0.5585 0.5610 0.5599 0.0010 0.17 5

0.2500 0.2545 0.2523 0.0017 0.67 5

0.0882 0.0896 0.0886 0.0006 0.65 5

0.0055 0.0056 0.0055 0.0000 0.65 5

554.00 612.00 576.20 22.05 3.83 5

18.559 20.441 19.336 0.754 3.90 5

18.699 20.495 19.463 0.691 3.55 5

FORM MP1116 (ASTMD2344) 2/29/2008

20

Input:

Test Plan Prefix AITR

Test Plan # 1392

Material IMU

Test SBS

Cure Cycle LH

Condition RTD 0.0055 16 Ultimate Load, lb. 413.00 420.00 419.00 422.00 394.00 NT NT NT NT NT

Test Group: AITR1392-IMU-SBS-LH-RTD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-SBS-C-LH1-RTD-1 AITR1392-IMU-SBS-C-LH1-RTD-2 AITR1392-IMU-SBS-C-LH1-RTD-3 AITR1392-IMU-SBS-C-LH1-RTD-4 AITR1392-IMU-SBS-C-LH1-RTD-5 AITR1392-IMU-SBS-C-LH2-RTD-1 AITR1392-IMU-SBS-C-LH2-RTD-2 AITR1392-IMU-SBS-C-LH2-RTD-3 AITR1392-IMU-SBS-C-LH2-RTD-4 AITR1392-IMU-SBS-C-LH2-RTD-5 Short Beam Shear MP1116 (ASTMD2344) Length, in. 0.562 0.562 0.562 0.561 0.560

Normalization: Cured Ply Thickness: Condition: RTD #Plies: Span (4t): 0.35 Cured Ply Width, in. Thickness, in. Thickness: 0.2525 0.0882 0.0055 0.2510 0.0888 0.0055 0.2525 0.0880 0.0055 0.2535 0.0875 0.0055 0.2520 0.0881 0.0055

ACG, Inc. Material & Process Laboratory Report
Failure Mode ILS ILS ILS ILS ILS Ultimate Strength, ksi Measured Normalized 13.909 13.940 14.138 14.261 14.137 14.143 14.269 14.188 13.310 13.325

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result FM=Failure Mode Unacceptable

0.5600 0.5615 0.5611 0.0007 0.12 5

0.2510 0.2535 0.2523 0.0009 0.36 5

0.0875 0.0888 0.0881 0.0005 0.51 5

0.0055 0.0055 0.0055 0.0000 0.51 5

394.00 422.00 413.60 11.46 2.77 5

13.310 14.269 13.953 0.382 2.74 5

13.325 14.261 13.971 0.380 2.72 5

FORM MP1116 (ASTMD2344) 2/29/2008

21

Input:

Test Plan Prefix AITR

Test Plan # 1392

Material IMU

Test SBS

Cure Cycle LH

Condition ETD 0.0055 16 Ultimate Load, lb. 315.00 317.00 322.00 311.00 311.00 NT NT NT NT NT

Test Group: AITR1392-IMU-SBS-LH-ETD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-SBS-C-LH1-ETD-1 AITR1392-IMU-SBS-C-LH1-ETD-2 AITR1392-IMU-SBS-C-LH1-ETD-3 AITR1392-IMU-SBS-C-LH1-ETD-4 AITR1392-IMU-SBS-C-LH1-ETD-5 AITR1392-IMU-SBS-C-LH2-ETD-1 AITR1392-IMU-SBS-C-LH2-ETD-2 AITR1392-IMU-SBS-C-LH2-ETD-3 AITR1392-IMU-SBS-C-LH2-ETD-4 AITR1392-IMU-SBS-C-LH2-ETD-5 Short Beam Shear MP1116 (ASTMD2344) Length, in. 0.561 0.561 0.559 0.563 0.561

Normalization: Cured Ply Thickness: Condition: ETD #Plies: Span (4t): 0.36 Cured Ply Width, in. Thickness, in. Thickness: 0.2530 0.0877 0.0055 0.2500 0.0891 0.0056 0.2530 0.0882 0.0055 0.2495 0.0894 0.0056 0.2500 0.0895 0.0056

ACG, Inc. Material & Process Laboratory Report
Failure Mode ILS ILS ILS ILS ILS Ultimate Strength, ksi Measured Normalized 10.644 10.611 10.673 10.807 10.818 10.847 10.453 10.624 10.425 10.602

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result FM=Failure Mode Unacceptable

0.5590 0.5625 0.5609 0.0012 0.22 5

0.2495 0.2530 0.2511 0.0017 0.70 5

0.0877 0.0895 0.0888 0.0008 0.88 5

0.0055 0.0056 0.0056 0.0000 0.88 5

311.00 322.00 315.20 4.60 1.46 5

10.425 10.818 10.603 0.164 1.54 5

10.602 10.847 10.698 0.119 1.11 5

FORM MP1116 (ASTMD2344) 2/29/2008

22

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test OHT1

Cure Cycle LH

Condition RTD Cured Ply Thickness: #Plies: 24 Diameter 0.2523 0.2522 0.2521 0.2520 0.2516 0.2508 0.2525 0.2510 0.2524 0.2519 Width/ Diameter 5.9555 5.9584 5.9636 5.9536 5.9613 5.9872 5.9447 5.9833 5.9527 5.9656 0.0055

Test Group: AITR1392-IMU-OHT1-LH-RTD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-OHT1-C-LH1-RTD-1 AITR1392-IMU-OHT1-C-LH1-RTD-2 AITR1392-IMU-OHT1-C-LH1-RTD-3 AITR1392-IMU-OHT1-C-LH1-RTD-4 AITR1392-IMU-OHT1-C-LH1-RTD-5 AITR1392-IMU-OHT1-C-LH2-RTD-1 AITR1392-IMU-OHT1-C-LH2-RTD-2 AITR1392-IMU-OHT1-C-LH2-RTD-3 AITR1392-IMU-OHT1-C-LH2-RTD-4 AITR1392-IMU-OHT1-C-LH2-RTD-5 Open-Hole Tension Layup 1 MP1117 (ASTMD5766) Length, in 12.0007 12.0006 12.0006 12.0001 12.0004 12.0018 12.0013 12.0019 12.0025 12.0007 Width, in 1.5026 1.5027 1.5034 1.5003 1.4999 1.5016 1.5010 1.5018 1.5025 1.5027

Normalization: NA Condition: RTD Thickness, in 0.1315 0.1308 0.1314 0.1309 0.1305 0.1333 0.1329 0.1323 0.1332 0.1334 Cured Ply Thickness: 0.0055 0.0055 0.0055 0.0055 0.0054 0.0056 0.0055 0.0055 0.0055 0.0056

ACG, Inc. Material & Process Laboratory Report
Ultimate Load, lb 12898.49 14958.76 13052.83 12969.63 NT 13735.34 13202.53 13320.77 13347.21 NT Ultimate Failure Mode Strength, ksi 65.28 AGM 76.11 AGM 66.06 AGM 66.04 AGM 68.64 66.17 67.07 66.70 AGM AGM AGM AGM

Diameter/ Thickness 1.9186 1.9281 1.9181 1.9251 1.9287 1.8819 1.8997 1.8979 1.8951 1.8878

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result NA=Not Applicable FM=Failure Mode Unacceptable

12.0001 12.0025 12.0011 0.0008 0.01 10

1.4999 1.5034 1.5019 0.0012 0.08 10

0.1305 0.1334 0.1320 0.0011 0.86 10

0.0054 0.0056 0.0055 0.0000 0.86 10

0.2508 0.2525 0.2519 0.0006 0.23 10

5.9447 5.9872 5.9626 0.0134 0.22 10

1.8819 1.9287 1.9081 0.0175 0.92 10

12898.4860 14958.7620 13435.6939 669.4695 4.98 8

65.2799 76.1054 67.7581 3.5161 5.19 8

FORM MP1117 (ASTMD5766) 2/29/2008

23

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 IMU

Test OHC1

Cure Cycle Condition LH RTD Cured Ply Thickness: #Plies: 24 0.0055

Test Group: AITR1392-IMU-OHC1-LH-RTD Material: MTM45-1/IM7-145-32%RW
Test Type: Test Method: Specimen ID AITR1392-IMU-OHC1-C-LH1-RTD-1 AITR1392-IMU-OHC1-C-LH1-RTD-2 AITR1392-IMU-OHC1-C-LH1-RTD-3 AITR1392-IMU-OHC1-C-LH1-RTD-4 AITR1392-IMU-OHC1-C-LH1-RTD-5 AITR1392-IMU-OHC1-C-LH2-RTD-1 AITR1392-IMU-OHC1-C-LH2-RTD-2 AITR1392-IMU-OHC1-C-LH2-RTD-3 AITR1392-IMU-OHC1-C-LH2-RTD-4 AITR1392-IMU-OHC1-C-LH2-RTD-5 Open-Hole Compression Layup 1 MP1119 (ASTMD6484) Length, in Width, in 11.9965 11.9963 11.9958 11.9966 11.9964 1.5056 1.5047 1.5049 1.5046 1.5051

Normalization: NA Condition: RTD

ACG, Inc. Material & Process Laboratory Report
Diameter/ Thickness 1.8753 1.8823 1.8750 1.8732 1.8749 Ultimate Load, lb 7140.00 7121.00 7219.00 7224.00 7000.00 NT NT NT NT NT Ultimate Strength, ksi 35.21 35.33 35.63 35.66 34.63 Failure Mode LGM LGM LGM LGM LGM

Thickness, Cured Ply Hole Edge- Hole Edge- Width/ Diameter Diameter Side (f) End (g) in Thickness: 0.6235 5.864 0.1347 0.0056 0.2526 5.9603 0.6235 5.8675 0.1339 0.0056 0.2521 5.9688 0.6255 5.866 0.1346 0.0056 0.2524 5.9624 0.6251 5.8665 0.1346 0.0056 0.2522 5.9660 0.6243 5.866 0.1343 0.0056 0.2518 5.9775

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested or Excluded NR=No Result NA=Not Applicable FM=Failure Mode Unacceptable

11.9958 11.9966 11.9963 0.0003 0.00 5

1.5046 1.5056 1.5050 0.0004 0.02 5

0.1339 0.1347 0.1344 0.0003 0.24 5

0.0056 0.0056 0.0056 0.0000 0.24 5

0.2518 0.2526 0.2522 0.0003 0.12 5

0.6235 0.6255 0.6244 0.0009 0.15 5

5.8640 5.8675 5.8660 0.0013 0.02 5

5.9603 5.9775 5.9670 0.0067 0.11 5

1.8732 1.8823 1.8761 0.0035 0.19 5

7000.0000 7224.0000 7140.8000 91.1795 1.28 5

34.6296 35.6611 35.2933 0.4187 1.19 5

FORM MP1119 (ASTMD6484) 2/29/2008

24

Material:
Test Type: Test Method: Specimen ID

MTM45-1/GF0103-35%RW
Warp Tensile MP1112 (ASTMD3039)

Normalization: Condition:

Cured Ply Thickness: CTD

0.01

#Plies:

12

AITR1392-8HG-WT-A-MH1-CTD-1 AITR1392-8HG-WT-A-MH1-CTD-2 AITR1392-8HG-WT-A-MH1-CTD-3 AITR1392-8HG-WT-A-MH1-CTD-4 AITR1392-8HG-WT-A-MH2-CTD-1 AITR1392-8HG-WT-A-MH2-CTD-2 AITR1392-8HG-WT-A-MH2-CTD-3 AITR1392-8HG-WT-A-MH2-CTD-4 AITR1392-8HG-WT-B-MH1-CTD-1 AITR1392-8HG-WT-B-MH1-CTD-2 AITR1392-8HG-WT-B-MH1-CTD-3 AITR1392-8HG-WT-B-MH1-CTD-4 AITR1392-8HG-WT-B-MH2-CTD-1 AITR1392-8HG-WT-B-MH2-CTD-2 AITR1392-8HG-WT-B-MH2-CTD-3 AITR1392-8HG-WT-B-MH2-CTD-4 AITR1392-8HG-WT-C-MH1-CTD-1 AITR1392-8HG-WT-C-MH1-CTD-2 AITR1392-8HG-WT-C-MH1-CTD-3 AITR1392-8HG-WT-C-MH1-CTD-4 AITR1392-8HG-WT-C-MH2-CTD-1 AITR1392-8HG-WT-C-MH2-CTD-2 AITR1392-8HG-WT-C-MH2-CTD-3 AITR1392-8HG-WT-C-MH2-CTD-4

Modulus/Poisson's Range: Thickness, Cured Ply Length, in. Width, in. in. Thickness: 10.004 1.0050 0.1157 0.0096 9.996 1.0060 0.1167 0.0097 10.004 1.0060 0.1158 0.0097 9.997 1.0060 0.1194 0.0100 10.004 1.0060 0.1332 0.0111 10.003 1.0060 0.1338 0.0112 10.000 1.0060 0.1306 0.0109 10.002 1.0050 0.1344 0.0112 9.996 1.0000 0.1170 0.0098 10.004 1.0040 0.1190 0.0099 10.002 1.0050 0.1190 0.0099 9.996 1.0040 0.1200 0.0100 10.000 1.0060 0.1210 0.0101 10.000 1.0070 0.1200 0.0100 9.998 1.0060 0.1200 0.0100 10.000 1.0070 0.1190 0.0099 10.000 1.0060 0.1209 0.0101 10.004 1.0060 0.1212 0.0101 9.997 1.0080 0.1198 0.0100 9.997 1.0070 0.1180 0.0098 9.998 1.0070 0.1195 0.0100 9.994 1.0070 0.1191 0.0099 10.000 1.0070 0.1192 0.0099 10.000 1.0070 0.1179 0.0098

Chord 0.1% to 0.3% Ultimate Failure Mode Load, lb. 9896.00 LAT 9907.00 LGT 10144.00 LAT NT 11010.00 LAT 10696.00 LAT 10815.00 LWT NT 9589.00 LAT 9843.00 LAT 9695.00 LWT NT 8913.00 DGM 9070.00 DGM/AGT 9103.00 LAT NT 9497.00 LWT 9131.00 DGM/LAT 9880.00 LWT NT 9343.00 LWT 9587.00 LAT 9607.00 LAT NT

ACG, Inc. Material & Process Laboratory Report
Poisson’s Ratio

Ultimate Strength, ksi Modulus, Msi Measured Normalized Measured Normalized 85.106 82.056 3.73 3.60 84.387 81.363 3.77 3.67 87.077 83.957 3.87 3.73 NT 82.165 79.220 3.58 3.97 79.463 76.616 3.64 4.06 82.316 79.367 3.76 4.10 NT 81.957 79.020 3.92 3.82 82.385 79.433 3.85 3.82 81.065 78.160 3.93 3.89 NT 73.222 70.598 3.81 3.84 75.058 72.368 3.98 3.98 75.406 72.704 3.90 3.90 NT 78.084 75.286 3.63 3.66 74.889 72.205 3.73 3.77 81.816 78.885 3.74 3.73 NT 77.641 74.858 3.67 3.65 79.936 77.071 3.75 3.73 80.035 77.167 3.84 3.81 NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

9.9940 10.0040 9.9998 0.0031 0.03 24

1.0000 1.0080 1.0058 0.0016 0.16 24

0.1157 0.1344 0.1213 0.0056 4.61 24

0.0096 0.0112 0.0101 0.0005 4.61 24

8913.00 11010.00 9762.56 599.56 6.14 18

73.222 87.077 80.112 3.806 4.75 18

70.598 83.957 77.241 3.670 4.75 18

3.578 3.984 3.784 0.113 2.98 18

3.600 4.097 3.819 0.143 3.74 18

B-MH2-4 Modulus from 1150 to 3150

FORM MP1112 (ASTMD3039) 2/29/2008

25

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 PWC1

Test WT

Cure Cycle Condition MH CTD

Test Group: AITR1392-PWC1-WT-MH-CTD MTM45-1/CF0525-36%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-PWC1-WT-A-MH1-CTD-1 AITR1392-PWC1-WT-A-MH1-CTD-2 AITR1392-PWC1-WT-A-MH1-CTD-3 AITR1392-PWC1-WT-A-MH1-CTD-4 AITR1392-PWC1-WT-A-MH2-CTD-1 AITR1392-PWC1-WT-A-MH2-CTD-2 AITR1392-PWC1-WT-A-MH2-CTD-3 AITR1392-PWC1-WT-A-MH2-CTD-4 AITR1392-PWC1-WT-B-MH1-CTD-1 AITR1392-PWC1-WT-B-MH1-CTD-2 AITR1392-PWC1-WT-B-MH1-CTD-3 AITR1392-PWC1-WT-B-MH1-CTD-4 AITR1392-PWC1-WT-B-MH2-CTD-1 AITR1392-PWC1-WT-B-MH2-CTD-2 AITR1392-PWC1-WT-B-MH2-CTD-3 AITR1392-PWC1-WT-B-MH2-CTD-4 AITR1392-PWC1-WT-C-MH1-CTD-1 AITR1392-PWC1-WT-C-MH1-CTD-2 AITR1392-PWC1-WT-C-MH1-CTD-3 AITR1392-PWC1-WT-C-MH1-CTD-4 AITR1392-PWC1-WT-C-MH2-CTD-1 AITR1392-PWC1-WT-C-MH2-CTD-2 AITR1392-PWC1-WT-C-MH2-CTD-3 AITR1392-PWC1-WT-C-MH2-CTD-4 Warp Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0079 #Plies: 14 ACG, Inc. Condition: Material & Process CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.068 0.9976 0.1134 0.0081 15196.00 LAT 134.326 137.727 9.05 9.28 10.056 1.0085 0.1134 0.0081 11467.00 LAT 100.268 102.806 8.80 9.02 10.088 1.0082 0.1114 0.0080 11669.00 LAT 103.897 106.527 9.35 9.42 10.078 1.0080 0.1119 0.0080 11577.00 LAT 102.637 105.236 9.39 9.50 10.057 1.0048 0.1097 0.0078 15190.00 LAT 137.807 141.296 9.59 9.51 10.052 1.0053 0.1103 0.0079 16296.00 LAT 146.964 150.684 9.58 9.56 10.048 1.0046 0.1117 0.0080 14107.00 LAT 125.715 128.898 9.27 9.37 10.052 1.0053 0.1096 0.0078 16005.00 LAT 145.261 148.939 9.64 9.55 10.038 1.0077 0.1117 0.0080 14094.00 LAT 125.213 128.383 9.52 9.61 10.050 1.0077 0.1138 0.0081 14160.00 LAT 123.478 126.604 9.24 9.51 10.052 1.0078 0.1144 0.0082 14409.00 LAB 124.978 128.142 9.17 9.49 10.031 1.0068 0.1141 0.0082 13932.00 LAT 121.279 124.349 9.24 9.53 10.013 1.0083 0.1150 0.0082 15635.00 LAT 134.837 138.251 9.24 9.60 10.006 1.0084 0.1130 0.0081 14793.00 LGT 129.821 133.108 9.41 9.61 10.006 1.0083 0.1126 0.0080 15417.00 LGT 135.791 139.229 9.14 9.31 10.008 1.0085 0.1125 0.0080 NT NT 10.050 0.9975 0.1148 0.0082 15586.00 LGB/LAT 136.107 139.553 9.49 9.85 10.045 0.9970 0.1144 0.0082 14244.00 LAT 124.885 128.047 9.32 9.64 10.043 0.9970 0.1149 0.0082 14954.00 LAT 130.540 133.844 9.24 9.60 10.055 0.9972 0.1125 0.0080 NT NT 10.064 1.0080 0.1162 0.0083 15752.00 LGT 134.484 137.888 9.54 10.03 10.052 1.0081 0.1139 0.0081 13353.00 LAT 116.292 119.237 9.47 9.76 10.052 1.0077 0.1137 0.0081 14455.00 LAT 126.161 129.355 8.87 9.12 10.062 1.0078 0.1149 0.0082 NT NT

Poisson’s Ratio Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested NT Not Tested Not Tested Not Tested NT Not Tested Not Tested Not Tested NT

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0060 10.0880 10.0469 0.0212 0.21 24

0.9970 1.0085 1.0053 0.0043 0.43 24

0.1096 0.1162 0.1131 0.0017 1.54 24

0.0078 0.0083 0.0081 0.0001 1.54 24

11467.00 16296.00 14394.81 1401.67 9.74 21

100.268 146.964 126.702 12.678 10.01 21

102.806 150.684 129.910 12.999 10.01 21

8.800 9.635 9.312 0.226 2.43 21

9.023 10.026 9.516 0.226 2.37 21

FORM MP1112 (ASTMD3039) 2/29/2008

26

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 PWC1

Test WT

Cure Cycle Condition M CTD

Test Group: AITR1392-PWC1-WT-M-CTD MTM45-1/CF0525-36%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-PWC1-WT-C-M1-CTD-1 AITR1392-PWC1-WT-C-M1-CTD-2 AITR1392-PWC1-WT-C-M1-CTD-3 AITR1392-PWC1-WT-C-M1-CTD-4 AITR1392-PWC1-WT-C-M2-CTD-1 AITR1392-PWC1-WT-C-M2-CTD-2 AITR1392-PWC1-WT-C-M2-CTD-3 AITR1392-PWC1-WT-C-M2-CTD-4 Warp Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0079 #Plies: 14 ACG, Inc. Condition: Material & Process CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.082 1.0039 0.1137 0.0081 16433.00 XGT/XGB 143.968 148.003 8.53 8.77 10.080 1.0049 0.1136 0.0081 16134.00 XGM 141.332 145.294 NT 10.079 1.0025 0.1134 0.0081 16193.00 LGM/LAT 142.439 146.432 9.45 9.69 10.080 0.9951 0.1148 0.0082 16363.00 XGV 143.237 147.251 9.17 9.52 10.066 0.9953 0.1144 0.0082 16045.00 XGV 140.916 144.866 9.60 9.93 10.045 0.9953 0.1147 0.0082 15871.00 XGB/LAT 139.023 142.920 GE 144.331 148.377 9.34 9.69 10.048 0.9953 0.1147 0.0082 16477.00 XGV 10.064 1.0040 0.1144 0.0082 17013.00 XGV 148.123 152.274 9.85 10.19

Poisson’s Ratio Not Tested NT Not Tested Not Tested Not Tested GE Not Tested Not Tested

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0450 10.0820 10.0680 0.0149 0.15 8

0.9951 1.0049 0.9995 0.0046 0.46 8

0.1134 0.1148 0.1142 0.0006 0.49 8

0.0081 0.0082 0.0082 0.0000 0.49 8

15871.00 17013.00 16316.13 347.92 2.13 8

139.023 148.123 142.921 2.731 1.91 8

142.920 152.274 146.927 2.808 1.91 8

8.530 9.849 9.323 0.452 4.85 6

8.769 10.188 9.630 0.482 5.01 6

FORM MP1112 (ASTMD3039) 2/29/2008

27

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 PWC1

Test WT

Cure Cycle Condition LH CTD

Test Group: AITR1392-PWC1-WT-LH-CTD MTM45-1/CF0525-36%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-PWC1-WT-B-LH1-CTD-1 AITR1392-PWC1-WT-B-LH1-CTD-2 AITR1392-PWC1-WT-B-LH1-CTD-3 AITR1392-PWC1-WT-B-LH1-CTD-4 AITR1392-PWC1-WT-B-LH2-CTD-1 AITR1392-PWC1-WT-B-LH2-CTD-2 AITR1392-PWC1-WT-B-LH2-CTD-3 AITR1392-PWC1-WT-B-LH2-CTD-4 Warp Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0079 #Plies: 14 ACG, Inc. Condition: CTD Material & Process Modulus/Poisson's Range: Chord 0.1% to 0.3% Laboratory Report Thickness, Cured Ply Ultimate Ultimate Strength, ksi Modulus, Msi Failure Mode Length, in. Width, in. Measured Normalized Measured Normalized in. Thickness: Load, lb. 10.013 1.0044 0.1125 0.0080 15766.00 LAT 139.528 141.925 9.81 9.98 10.042 1.0051 0.1127 0.0081 14823.00 LGB/LAT 130.859 133.107 8.89 9.06 10.044 1.0051 0.1134 0.0081 15081.00 LGB/LAT 132.315 134.588 9.39 9.63 10.055 1.0052 0.1132 0.0081 15339.00 LAT/LAB 134.803 137.118 9.48 9.70 10.034 1.0093 0.1129 0.0081 15536.00 LAT 136.341 138.683 9.57 9.77 10.049 1.0100 0.1127 0.0081 15425.00 LAT 135.513 137.841 9.30 9.47 10.023 1.0098 0.1124 0.0080 15379.00 LAB 135.496 137.824 9.89 10.05 10.054 1.0097 0.1132 0.0081 14579.00 LGB 127.552 129.744 9.83 10.06

Poisson’s Ratio Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested Not Tested

Minimum Maximum Average Standard Deviation Coefficient of Variation (%) No. Specimens Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable

10.0130 10.0550 10.0393 0.0150 0.15 8

1.0044 1.0100 1.0073 0.0026 0.25 8

0.1124 0.1134 0.1129 0.0004 0.32 8

0.0080 0.0081 0.0081 0.0000 0.32 8

14579.00 15766.00 15241.00 389.82 2.56 8

127.552 139.528 134.051 3.693 2.75 8

129.744 141.925 136.354 3.756 2.75 8

8.895 9.890 9.520 0.334 3.50 8

9.063 10.061 9.715 0.337 3.47 8

WT-B-LH2-CTD-1: Modulus 1500 to 3500; WT-B-LH2-CTD-4: Modulus 2000 to 4000

FORM MP1112 (ASTMD3039) 2/29/2008

28

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 ASU1

Test LT

Cure Cycle Condition MH CTD

Test Group: AITR1392-ASU1-LT-MH-CTD MTM45-1/AS4-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-ASU1-LT-A-MH1-CTD-1 AITR1392-ASU1-LT-A-MH1-CTD-2 AITR1392-ASU1-LT-A-MH1-CTD-3 AITR1392-ASU1-LT-A-MH1-CTD-4 AITR1392-ASU1-LT-A-MH2-CTD-1 AITR1392-ASU1-LT-A-MH2-CTD-2 AITR1392-ASU1-LT-A-MH2-CTD-3 AITR1392-ASU1-LT-A-MH2-CTD-4 AITR1392-ASU1-LT-B-MH1-CTD-1 AITR1392-ASU1-LT-B-MH1-CTD-2 AITR1392-ASU1-LT-B-MH1-CTD-3 AITR1392-ASU1-LT-B-MH1-CTD-4 AITR1392-ASU1-LT-B-MH2-CTD-1 AITR1392-ASU1-LT-B-MH2-CTD-2 AITR1392-ASU1-LT-B-MH2-CTD-3 AITR1392-ASU1-LT-B-MH2-CTD-4 AITR1392-ASU1-LT-C-MH1-CTD-1 AITR1392-ASU1-LT-C-MH1-CTD-2 AITR1392-ASU1-LT-C-MH1-CTD-3 AITR1392-ASU1-LT-C-MH1-CTD-4 AITR1392-ASU1-LT-C-MH2-CTD-1 AITR1392-ASU1-LT-C-MH2-CTD-2 AITR1392-ASU1-LT-C-MH2-CTD-3 AITR1392-ASU1-LT-C-MH2-CTD-4 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 Condition: CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Failure Mode Ultimate Strength , ksi Length, in. Width, in. Measured Normalized in. Thickness: Load, lb. 10.032 1.0058 0.0895 0.0056 NT 251.048 253.568 10.038 1.0052 0.0920 0.0058 NT 260.450 268.392 10.037 1.0054 0.0909 0.0057 NT 262.286 269.489 10.040 1.0053 0.0893 0.0056 NT 278.123 279.861 10.036 0.9997 0.0862 0.0054 NT 290.524 291.734 10.031 1.0074 0.0903 0.0056 NT 229.338 235.984 10.039 1.0074 0.0909 0.0057 NT 255.635 260.912 10.032 1.0070 0.0879 0.0055 NT 10.031 1.0082 0.0891 0.0056 NT 10.031 1.0090 0.0884 0.0055 NT 10.037 1.0084 0.0885 0.0055 NT 252.770 256.983 10.032 1.0087 0.0877 0.0055 NT 257.881 259.053 10.036 1.0073 0.0814 0.0051 NT 287.969 278.752 10.039 1.0066 0.0842 0.0053 NT 255.858 254.162 10.041 1.0067 0.0819 0.0051 NT 286.222 275.217 10.035 1.0068 0.0853 0.0053 NT 285.013 277.834 10.067 1.0083 0.0840 0.0053 NT 284.023 277.407 10.064 1.0073 0.0841 0.0053 NT 263.728 258.184 10.066 1.0078 0.0834 0.0052 NT 251.952 244.985 10.067 1.0075 0.0860 0.0054 NT 286.682 283.696 10.064 1.0095 0.0881 0.0055 NT 292.729 287.961 10.068 1.0097 0.0888 0.0055 NT 255.609 255.899 10.065 1.0096 0.0856 0.0054 NT 247.651 244.977 10.063 1.0095 0.0862 0.0054 NT 266.673 262.178

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 17.43 17.73 19.34 20.22 19.24 19.88 NT 18.65 18.27 18.93 19.42 18.43 19.04 NT 18.28 18.50 19.17 19.26 18.69 18.79 NT 20.09 18.58 20.00 19.14 19.74 18.36 NT 18.39 17.55 18.79 17.96 19.62 18.59 NT 19.90 19.92 17.69 17.85 18.85 18.33 NT Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT NT

Minimum 10.0306 0.9997 Maximum 10.0678 1.0097 Average 10.0454 1.0073 Standard Deviation 0.0149 0.0021 Coefficient of Variation (%) 0.15 0.21 No. Specimens 24 24 Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable (1) Derived in accordance with AI/TR/1392 Table 3a , note (1)

0.0814 0.0920 0.0871 0.0029 3.35 24

0.0051 0.0058 0.0054 0.0002 3.35 24

229.338 292.729 266.770 17.560 6.58 21

235.984 291.734 265.582 15.156 5.71 21

17.426 20.093 18.956 0.758 4.00 18

17.550 20.217 18.744 0.779 4.16 18

FORM MP1112 (ASTMD3039) 2/29/2008

29

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 ASU1

Test LT

Cure Cycle Condition M CTD

Test Group: AITR1392-ASU1-LT-M-CTD MTM45-1/AS4-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-ASU1-LT-C-M1-CTD-1 AITR1392-ASU1-LT-C-M1-CTD-2 AITR1392-ASU1-LT-C-M1-CTD-3 AITR1392-ASU1-LT-C-M1-CTD-4 AITR1392-ASU1-LT-C-M1-CTD-5 AITR1392-ASU1-LT-C-M2-CTD-1 AITR1392-ASU1-LT-C-M2-CTD-2 AITR1392-ASU1-LT-C-M2-CTD-3 AITR1392-ASU1-LT-C-M2-CTD-4 AITR1392-ASU1-LT-C-M2-CTD-5 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 Condition: CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Failure Mode Ultimate Strength , ksi Length, in. Width, in. Measured Normalized in. Thickness: Load, lb. 10.065 1.0074 0.0859 0.0054 NT 279.970 277.478 10.065 1.0077 0.0867 0.0054 NT 285.536 284.455 10.067 1.0085 0.0851 0.0053 NT 282.186 277.911 10.063 1.0085 0.0853 0.0053 NT 10.068 1.0089 0.0864 0.0054 NT 280.152 278.667 10.064 1.0066 0.0846 0.0053 NT 281.016 275.108 10.067 1.0063 0.0845 0.0053 NT 279.547 271.076 10.061 1.0073 0.0837 0.0052 NT 291.998 283.316 10.064 1.0075 0.0829 0.0052 NT 275.252 264.044 10.067 1.0070 0.0856 0.0053 NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 18.72 18.27 19.30 19.01 19.17 18.54 20.01 19.39 NT 18.86 18.13 19.42 18.64 18.72 17.81 19.61 18.48 NT Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum 10.0610 1.0063 Maximum 10.0675 1.0089 Average 10.0650 1.0076 Standard Deviation 0.0021 0.0008 Coefficient of Variation (%) 0.02 0.08 No. Specimens 10 10 Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable (1) Derived in accordance with AI/TR/1392 Table 3a , note (1)

0.0829 0.0867 0.0851 0.0012 1.37 10

0.0052 0.0054 0.0053 0.0001 1.37 10

275.252 291.998 281.957 4.965 1.76 8

264.044 284.455 276.507 6.589 2.38 8

18.715 20.011 19.226 0.457 2.38 8

17.814 19.389 18.534 0.496 2.68 8

FORM MP1112 (ASTMD3039) 2/29/2008

30

Input:

Test Plan Prefix AITR

Test Plan # Material 1392 ASU1

Test LT

Cure Cycle Condition LH CTD

Test Group: AITR1392-ASU1-LT-LH-CTD MTM45-1/AS4-145-32%RW Normalization: Material:
Test Type: Test Method: Specimen ID AITR1392-ASU1-LT-B-LH1-CTD-1 AITR1392-ASU1-LT-B-LH1-CTD-2 AITR1392-ASU1-LT-B-LH1-CTD-3 AITR1392-ASU1-LT-B-LH1-CTD-4 AITR1392-ASU1-LT-B-LH1-CTD-5 AITR1392-ASU1-LT-B-LH2-CTD-1 AITR1392-ASU1-LT-B-LH2-CTD-2 AITR1392-ASU1-LT-B-LH2-CTD-3 AITR1392-ASU1-LT-B-LH2-CTD-4 AITR1392-ASU1-LT-B-LH2-CTD-5 Longitudinal Tensile MP1112 (ASTMD3039)

Cured Ply Thickness: 0.0055 #Plies: 16 Condition: CTD Modulus/Poisson's Range: Chord 0.1% to 0.3% (1) Thickness, Cured Ply Ultimate Failure Mode Ultimate Strength , ksi Length, in. Width, in. Measured Normalized in. Thickness: Load, lb. 10.067 1.0058 0.0869 0.0054 NT 288.704 285.751 10.067 1.0054 0.0815 0.0051 NT 292.094 280.311 10.071 1.0065 0.0841 0.0053 NT 293.000 289.559 10.070 1.0058 0.0822 0.0051 NT 270.642 262.185 10.070 1.0069 0.0861 0.0054 NT 10.029 1.0069 0.0827 0.0052 NT 289.361 281.360 10.034 1.0079 0.0836 0.0052 NT 266.012 259.865 10.029 1.0066 0.0833 0.0052 NT 282.884 277.151 10.027 1.0070 0.0845 0.0053 NT 283.113 281.182 10.025 1.0063 0.0810 0.0051 NT

ACG, Inc. Material & Process Laboratory Report
Modulus, Msi Measured Normalized 19.91 19.65 20.36 18.85 19.71 18.83 20.40 19.06 NT 19.99 18.78 19.67 18.69 19.28 18.26 20.12 19.32 NT Poisson’s Ratio NT NT NT NT NT NT NT NT NT NT

Minimum 10.0250 1.0054 Maximum 10.0710 1.0079 Average 10.0487 1.0065 Standard Deviation 0.0212 0.0007 Coefficient of Variation (%) 0.21 0.07 No. Specimens 10 10 Notes: NT=Not Tested NR=No Result GE=Gage Error FM=Failure Mode Unacceptable (1) Derived in accordance with AI/TR/1392 Table 3a , note (1)

0.0810 0.0869 0.0836 0.0019 2.24 10

0.0051 0.0054 0.0052 0.0001 2.24 10

266.012 293.000 283.226 9.976 3.52 8

259.865 289.559 277.171 10.655 3.84 8

19.284 20.402 19.930 0.374 1.88 8

18.261 19.650 18.930 0.419 2.21 8

FORM MP1112 (ASTMD3039) 2/29/2008

31

MP1504 PWC1 MTM45-1-CF0525-36%RW AITR1392-8HQ-WC-MH-CTD MTM45-1/4581-35% RW QUARTZ "WARP COMPRESSSION" Tested Cold/Dry @ -65°F

Testing completed as of 30 Jan 2006

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 107.1 112.1 NR 106.8 NR 110.0 110.4 107.1 101.0 105.8 94.1 106.6 92.7 106.0 102.7 106.4 90.5 88.5 88.4 88.3 85.4 88.7 89.5 88.4 98.93 9.2725 9.3730 85.37 112.10 22

Modulus Poisson's Msi Ratio 3.77 0.11 3.98 0.12 3.63 0.12 3.95 0.15 3.79 0.13 3.66 0.10 3.80 0.12 3.73 0.13 3.82 0.14 3.83 0.12 3.74 0.12 3.83 0.09 3.53 0.11 3.71 0.13 3.87 0.16 3.65 0.15 3.47 0.11 NR NR 3.86 0.14 3.48 0.13 3.45 0.12 3.27 0.10 3.62 0.13 3.99 0.16 3.7143 0.1836 4.9429 3.2700 3.9900 23 0.12565 0.0185 14.7581 0.0900 0.1600 23

Avg. Specimen Thickn. [in] 0.1210 0.1200 0.1210 0.1210 0.1200 0.1200 0.1200 0.1200 0.1240 0.1240 0.1220 0.1240 0.1230 0.1230 0.1240 0.1240 0.1260 0.1260 0.1260 0.1260 0.1240 0.1250 0.1240 0.1240 0.1230 0.0021 1.7454 0.1200 0.1260 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01008 0.01000 0.01008 0.01008 0.01000 0.01000 0.01000 0.01000 0.01033 0.01033 0.01017 0.01033 0.01025 0.01025 0.01033 0.01033 0.01050 0.01050 0.01050 0.01050 0.01033 0.01042 0.01033 0.01033 0.0103 0.0002 1.7454 0.0100 0.0105 24

Strengthnorm [ksi] 104.798 108.835 NR 104.583 NR 106.796 107.155 104.000 101.307 106.122 92.911 106.935 92.280 105.436 103.032 106.764 92.206 90.218 90.076 89.994 85.646 89.735 89.830 88.706 98.52 8.0655 8.1870 85.65 108.83 22

32

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WC-MH-RTD MTM45-1/4581-35% RW QUARTZ "WARP COMPRESSSION" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 92.85 90.17 95.52 93.28 86.32 97.20 90.41 86.40 91.75 91.28 91.57 92.82 74.22 75.33 76.69 78.27 76.69 79.76 86.70 7.6984 8.8797 74.22 97.20 18

Modulus Poisson's Msi Ratio 3.64 0.13 3.76 0.13 3.65 0.13 3.81 0.13 3.79 0.13 3.71 0.13 3.70 0.13 3.50 0.13 3.63 0.12 3.55 0.14 3.79 0.13 3.63 0.13 3.64 0.13 3.61 0.13 3.48 0.13 3.55 0.13 3.56 0.13 3.69 0.12 3.6494 0.0990 2.7134 3.4800 3.8100 18 0.1294 0.0042 3.2151 0.1200 0.1400 18

Avg. Specimen Thickn. [in] 0.1200 0.1200 0.1210 0.1200 0.1200 0.1200 0.1240 0.1240 0.1230 0.1240 0.1220 0.1240 0.1260 0.1260 0.1260 0.1250 0.1250 0.1250 0.1231 0.0023 1.9001 0.1200 0.1260 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.01000 0.01008 0.01000 0.01000 0.01000 0.01033 0.01033 0.01025 0.01033 0.01017 0.01033 0.01050 0.01050 0.01050 0.01042 0.01042 0.01042 0.0103 0.0002 1.9001 0.0100 0.0105 18

Strengthnorm [ksi] 90.146 87.544 93.511 90.563 83.806 94.369 90.703 86.680 91.305 91.575 90.385 93.120 75.661 76.793 78.179 79.157 77.559 80.663 86.21 6.5170 7.5598 75.66 94.37 18

33

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WC-MH-ETW MTM45-1/4581-35% RW QUARTZ "WARP COMPRESSSION" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 66.50 64.16 62.27 61.31 68.55 62.55 67.65 58.66 62.42 64.82 61.78 59.23 64.17 60.59 60.48 61.18 49.72 52.57 48.45 50.51 50.05 51.37 52.11 51.26 58.85 6.3355 10.7658 48.45 68.55 24

Modulus Poisson's Msi Ratio 3.69 0.12 3.66 0.09 3.79 0.12 4.06 0.14 3.83 0.12 3.75 0.12 3.92 0.15 3.79 0.12 NR NR 3.80 0.13 3.85 0.13 4.45 0.15 3.81 0.12 3.74 0.13 3.78 0.12 3.88 0.13 NR NR NR NR 3.92 0.13 3.54 0.12 3.94 0.13 3.76 0.13 3.83 0.13 NR NR 3.8395 0.1815 4.7264 3.5400 4.4500 20 0.1265 0.0127 10.0239 0.0900 0.1500 20

Avg. Specimen Thickn. [in] 0.1220 0.1200 0.1210 0.1220 0.1200 0.1200 0.1190 0.1200 0.1240 0.1240 0.1240 0.1250 0.1240 0.1220 0.1240 0.1230 0.1260 0.1240 0.1250 0.1260 0.1240 0.1240 0.1220 0.1260 0.1230 0.0021 1.7207 0.1190 0.1260 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.01000 0.01008 0.01017 0.01000 0.01000 0.00992 0.01000 0.01033 0.01033 0.01033 0.01042 0.01033 0.01017 0.01033 0.01025 0.01050 0.01033 0.01042 0.01050 0.01033 0.01033 0.01017 0.01050 0.0102 0.0002 1.7207 0.0099 0.0105 24

Strengthnorm [ksi] 65.639 62.291 60.960 60.516 66.553 60.728 65.132 56.951 62.622 65.030 61.980 59.901 64.378 59.806 60.676 60.883 50.685 52.740 48.999 51.491 50.212 51.536 51.435 52.255 58.48 5.7171 9.7769 49.00 66.55 24

34

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WC-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "WARP COMPRESSSION" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 54.87 56.61 57.12 58.17 54.90 54.09 55.50 53.64 53.66 54.93 53.60 56.22 51.60 54.73 52.60 52.39 44.34 45.65 55.87 45.36 45.22 45.08 46.32 45.65 52.01 4.5960 8.8376 44.34 58.17 24

Modulus Poisson's Msi Ratio 3.76 0.11 NR NR NR NR NR NR 3.91 0.11 NR NR 4.25 0.13 NR NR NR NR 4.14 0.16 4.27 0.11 NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR NR 4.0660 0.2230 5.4846 3.7600 4.2700 5 0.1240 0.0219 17.6685 0.1100 0.1600 5

Avg. Specimen Thickn. [in] 0.1190 0.1220 0.1200 0.1210 0.1200 0.1170 0.1200 0.1200 0.1250 0.1250 0.1240 0.1240 0.1230 0.1230 0.1240 0.1230 0.1260 0.1260 0.1240 0.1250 0.1250 0.1250 0.1220 0.1240 0.1228 0.0024 1.9800 0.1170 0.1260 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00992 0.01017 0.01000 0.01008 0.01000 0.00975 0.01000 0.01000 0.01042 0.01042 0.01033 0.01033 0.01025 0.01025 0.01033 0.01025 0.01050 0.01050 0.01033 0.01042 0.01042 0.01042 0.01017 0.01033 0.0102 0.0002 1.9800 0.0098 0.0105 24

Strengthnorm [ksi] 52.828 55.877 55.456 56.946 53.301 51.202 53.883 52.078 54.268 55.552 53.773 56.402 51.350 54.464 52.770 52.136 45.201 46.536 56.051 45.874 45.732 45.591 45.720 45.798 51.62 4.1186 7.9794 45.20 56.95 24

35

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FC-MH-CTD MTM45-1/4581-35% RW QUARTZ "FILL COMPRESSSION" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 97.52 96.98 97.66 NR 111.54 NR 104.10 NR 84.29 85.51 85.69 92.41 84.66 86.99 87.08 80.55 91.70 89.96 93.23 85.47 91.13 90.59 86.90 91.39 91.21 7.2653 7.9657 80.55 111.54 21

Modulus Poisson's Msi Ratio 3.47 0.11 3.46 0.11 3.71 0.15 3.58 0.12 4.11 0.11 NR NR 3.86 0.16 3.66 0.08 3.51 0.16 3.68 0.15 3.65 0.15 3.64 0.12 3.32 0.11 3.68 0.15 3.58 0.13 3.53 0.14 3.66 0.18 3.34 0.15 2.97 0.10 3.36 0.16 3.82 0.17 3.43 0.12 3.50 0.15 3.37 0.11 3.5604 0.2255 6.3340 2.9700 4.1100 23 0.1343 0.0257 19.1521 0.0800 0.1800 23

Avg. Specimen Thickn. [in] 0.1210 0.1230 0.1240 0.1210 0.1150 0.1220 0.1190 0.1190 0.1280 0.1240 0.1280 0.1250 0.1200 0.1210 0.1240 0.1240 0.1220 0.1280 0.1260 0.1290 0.1240 0.1270 0.1250 0.1280 0.1236 0.0035 2.8405 0.1150 0.1290 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01008 0.01025 0.01033 0.01008 0.00958 0.01017 0.00992 0.00992 0.01067 0.01033 0.01067 0.01042 0.01000 0.01008 0.01033 0.01033 0.01017 0.01067 0.01050 0.01075 0.01033 0.01058 0.01042 0.01067 0.0103 0.0003 2.8405 0.0096 0.0108 24

Strengthnorm [ksi] 95.469 96.509 97.976 NR 103.779 NR 100.226 NR 87.291 85.787 88.740 93.457 82.194 85.160 87.362 80.811 90.513 93.162 95.040 89.204 91.425 93.082 87.884 94.643 91.41 5.8161 6.3623 80.81 103.78 21

36

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FC-MH-RTD MTM45-1/4581-35% RW QUARTZ "FILL COMPRESSSION" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 81.63 85.04 80.69 93.21 96.16 94.31 71.69 70.33 71.14 72.62 76.31 73.29 78.79 78.55 76.60 73.71 75.95 73.33 79.08 8.1288 10.2798 70.33 96.16 18

Modulus Poisson's Msi Ratio 3.54 0.12 3.76 0.13 3.76 0.12 3.62 0.13 3.58 0.13 3.65 0.13 3.38 0.11 3.53 0.12 3.60 0.12 3.37 0.13 3.45 0.12 3.47 0.13 3.25 0.13 3.20 0.13 3.25 0.12 3.22 0.12 3.09 0.13 3.4 0.13 3.4511 0.1962 5.6841 3.0900 3.7600 18 0.1250 0.0062 4.9468 0.1100 0.1300 18

Avg. Specimen Thickn. [in] 0.1220 0.1200 0.1200 0.1190 0.1190 0.1190 0.1240 0.1200 0.1240 0.1270 0.1280 0.1260 0.1270 0.1270 0.1290 0.1310 0.1300 0.1300 0.1246 0.0043 3.4529 0.1190 0.1310 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.01000 0.01000 0.00992 0.00992 0.00992 0.01033 0.01000 0.01033 0.01058 0.01067 0.01050 0.01058 0.01058 0.01075 0.01092 0.01083 0.01083 0.0104 0.0004 3.4529 0.0099 0.0109 18

Strengthnorm [ksi] 80.573 82.563 78.340 89.741 92.581 90.800 71.922 68.282 71.370 74.618 79.027 74.713 80.957 80.711 79.947 78.123 79.883 77.127 79.52 6.5232 8.2036 68.28 92.58 18

37

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FC-MH-ETD MTM45-1/4581-35% RW QUARTZ "FILL COMPRESSSION" Tested DRY @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 66.79 68.94 64.32 69.00 78.96 81.19 76.28 76.84 63.21 63.09 62.18 62.56 61.55 60.57 61.89 62.68 65.16 67.53 70.43 67.80 66.68 64.35 69.88 65.80 67.40 5.7475 8.5270 60.57 81.19 24

Modulus Poisson's Msi Ratio NR NR 4.05 0.130 NR NR 4.00 0.130 NR NR NR NR NR NR 3.83 0.130 3.70 0.120 NR NR NR NR 3.88 0.120 NR NR 4.13 0.110 3.78 0.130 NR NR 3.57 0.120 3.65 0.130 3.70 0.110 NR NR 3.50 0.130 3.56 0.120 3.81 0.130 3.71 NR 3.7764 0.1886 4.9947 3.5000 4.1300 14 0.1238 0.0077 6.2008 0.1100 0.1300 13

Avg. Specimen Thickn. [in] 0.1220 0.1220 0.1240 0.1240 0.1190 0.1200 0.1220 0.1200 0.1200 0.1250 0.1270 0.1240 0.1190 0.1190 0.1240 0.1220 0.1270 0.1280 0.1240 0.1270 0.1300 0.1280 0.1250 0.1270 0.1237 0.0033 2.6273 0.1190 0.1300 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.01017 0.01033 0.01033 0.00992 0.01000 0.01017 0.01000 0.01000 0.01042 0.01058 0.01033 0.00992 0.00992 0.01033 0.01017 0.01058 0.01067 0.01033 0.01058 0.01083 0.01067 0.01042 0.01058 0.0103 0.0003 2.6273 0.0099 0.0108 24

Strengthnorm [ksi] 65.925 68.048 64.528 69.223 76.021 78.825 75.293 74.602 61.369 63.805 63.890 62.762 59.259 58.316 62.090 61.869 66.952 69.934 70.658 69.665 70.133 66.641 70.672 67.610 67.420 5.3773 7.9757 58.32 78.83 24

38

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FC-MH-ETW MTM45-1/4581-35% RW QUARTZ "FILL COMPRESSSION" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 58.79 55.25 52.66 54.24 62.83 66.03 65.41 61.34 45.51 46.30 45.51 47.21 46.74 47.10 47.52 49.55 43.88 45.19 46.14 46.33 45.22 42.59 47.74 47.33 50.68 7.1397 14.0867 42.59 66.03 24

Modulus Poisson's Msi Ratio 3.87 0.17 NR NR 3.91 0.15 3.67 0.13 NR NR 3.77 0.11 3.65 0.11 3.91 0.12 4.00 0.13 3.38 0.13 3.64 0.13 4.17 0.17 3.41 0.11 3.69 0.12 3.57 0.13 3.43 0.12 3.64 0.11 3.20 0.13 3.39 0.11 4.00 0.14 3.47 0.12 NR NR 3.53 0.12 4.12 0.12 3.6867 0.2656 7.2033 3.2000 4.1700 21 0.1276 0.0176 13.7752 0.1100 0.1700 21

Avg. Specimen Thickn. [in] 0.1240 0.1240 0.1240 0.1230 0.1180 0.1190 0.1210 0.1200 0.1250 0.1250 0.1230 0.1260 0.1240 0.1240 0.1200 0.1230 0.1190 0.1290 0.1260 0.1210 0.1300 0.1310 0.1280 0.1290 0.1240 0.0036 2.9126 0.1180 0.1310 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01033 0.01033 0.01025 0.00983 0.00992 0.01008 0.01000 0.01042 0.01042 0.01025 0.01050 0.01033 0.01033 0.01000 0.01025 0.00992 0.01075 0.01050 0.01008 0.01083 0.01092 0.01067 0.01075 0.0103 0.0003 2.9126 0.0098 0.0109 24

Strengthnorm [ksi] 58.980 55.429 52.830 53.977 59.983 63.573 64.034 59.553 46.025 46.824 45.289 48.127 46.891 47.252 46.136 49.309 42.247 47.164 47.036 45.355 47.561 45.140 49.439 49.398 50.73 6.2768 12.3726 42.25 64.03 24

39

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FC-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "FILL COMPRESSSION" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 50.23 46.15 51.43 49.87 50.48 54.76 53.51 56.49 40.81 41.86 40.39 41.66 43.03 42.11 43.65 43.45 38.04 39.78 42.17 38.61 42.38 41.30 40.57 39.92 44.69 5.4693 12.2374 38.04 56.49 24

Modulus Poisson's Msi Ratio NR NR NR NR NR NR 4.03 0.11 4.26 0.11 NR NR NR NR 4.07 0.12 NR NR NR NR NR NR 3.53 0.11 NR NR NR NR 3.72 0.11 3.66 0.12 NR NR 3.90 0.13 4.48 0.14 NR NR 4.59 0.14 NR NR NR NR NR NR 4.0267 0.3658 9.0841 3.5300 4.5900 9 0.1211 0.0127 10.4804 0.1100 0.1400 9

Avg. Specimen Thickn. [in] 0.1220 0.1180 0.1220 0.1210 0.1190 0.1200 0.1190 0.1220 0.1200 0.1240 0.1240 0.1240 0.1220 0.1260 0.1240 0.1260 0.1210 0.1290 0.1250 0.1280 0.1290 0.1240 0.1290 0.1280 0.1236 0.0034 2.7406 0.1180 0.1290 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.00983 0.01017 0.01008 0.00992 0.01000 0.00992 0.01017 0.01000 0.01033 0.01033 0.01033 0.01017 0.01050 0.01033 0.01050 0.01008 0.01075 0.01042 0.01067 0.01075 0.01033 0.01075 0.01067 0.0103 0.0003 2.7406 0.0098 0.0108 24

Strengthnorm [ksi] 49.580 44.059 50.764 48.821 48.601 53.165 51.519 55.759 39.621 41.995 40.521 41.795 42.473 42.928 43.791 44.294 37.240 41.518 42.648 39.984 44.232 41.434 42.342 41.341 44.60 4.7616 10.6760 37.24 55.76 24

40

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNC1-MH-RTD MTM45-1/4581-35% RW QUARTZ "UNNOTCHED COMPRESSSION" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 74.26 74.42 73.08 76.18 77.26 77.88 75.10 71.21 75.99 74.56 74.96 68.80 71.33 67.48 71.64 70.25 71.81 71.31 73.20 2.8943 3.9542 67.48 77.88 18

Modulus Poisson's Msi Ratio 3.67 0.30 3.15 0.27 3.06 0.28 2.97 0.26 3.04 0.28 3.03 0.28 2.84 0.29 2.63 0.30 2.96 0.30 2.96 0.27 2.91 0.28 3.12 0.28 2.85 0.27 2.98 0.28 2.93 0.28 2.92 0.28 2.84 0.28 2.89 0.27 2.9861 0.2079 6.9634 2.6300 3.6700 18 0.2806 0.0111 3.9563 0.2600 0.3000 18

Avg. Specimen Thickn. [in] 0.1170 0.1160 0.1160 0.1160 0.1180 0.1170 0.1230 0.1240 0.1240 0.1220 0.1220 0.1200 0.1250 0.1250 0.1250 0.1220 0.1220 0.1220 0.1209 0.0034 2.7784 0.1160 0.1250 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00975 0.00967 0.00967 0.00967 0.00983 0.00975 0.01025 0.01033 0.01033 0.01017 0.01017 0.01000 0.01042 0.01042 0.01042 0.01017 0.01017 0.01017 0.0101 0.0003 2.7784 0.0097 0.0104 18

Strengthnorm [ksi] 70.295 69.844 68.586 71.496 73.760 73.721 74.735 71.440 76.236 73.595 73.990 66.796 72.138 68.244 72.451 69.341 70.880 70.387 71.55 2.5028 3.4979 66.80 76.24 18

41

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNC1-MH-ETW MTM45-1/4581-35% RW QUARTZ "UNNOTCHED COMPRESSSION" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8

ACG Batch # D D D D A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 48.52 52.05 53.89 53.34 52.04 47.58 50.98 54.21 51.58 2.4351 4.7213 47.58 54.21 8

Modulus Poisson's Msi Ratio 3.03 0.34 2.90 0.31 3.43 0.30 3.07 0.32 3.03 0.31 3.18 0.28 3.07 0.30 3.46 0.40 3.1463 0.1998 6.3498 2.9000 3.4600 8 0.3200 0.0366 11.4516 0.2800 0.4000 8

Avg. Specimen Thickn. [in] 0.1160 0.1160 0.1170 0.1160 0.1180 0.1170 0.1170 0.1180 0.1169 0.0008 0.7140 0.1160 0.1180 8

# Plies in Laminate 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00967 0.00967 0.00975 0.00967 0.00983 0.00975 0.00975 0.00983 0.0097 0.0001 0.7140 0.0097 0.0098 8

Strengthnorm [ksi] 45.537 48.850 51.012 50.060 49.682 45.039 48.258 51.754 48.77 2.4222 4.9662 45.04 51.75 8

42

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNC1-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "UNNOTCHED COMPRESSSION" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 46.68 45.55 46.43 45.08 45.53 44.75 44.72 42.43 43.07 42.50 42.77 44.09 43.95 43.59 43.24 41.36 39.19 37.97 39.87 37.34 38.29 39.15 39.70 39.19 42.35 2.8617 6.7569 37.34 46.68 24

Modulus Poisson's Msi Ratio 4.50 0.49 3.15 0.35 4.14 0.47 NR NR NR NR NR NR NR NR NR NR 3.98 0.41 3.70 0.39 4.53 0.48 3.54 0.39 3.67 0.45 NR NR NR NR NR NR 4.02 0.45 3.56 0.39 4.00 0.41 NR NR NR N\ NR N 3.50 N 3.49 0.37 3.8292 0.4092 10.6850 3.1500 4.5300 13 0.4208 0.0458 10.8873 0.3500 0.4900 12

Avg. Specimen Thickn. [in] 0.1150 0.1170 0.1170 0.1160 0.1180 0.1170 0.1150 0.1150 0.1220 0.1210 0.1220 0.1220 0.1230 0.1240 0.1240 0.1240 0.1250 0.1250 0.1250 0.1250 0.1220 0.1220 0.1220 0.1220 0.1208 0.0036 2.9454 0.1150 0.1250 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00958 0.00975 0.00975 0.00967 0.00983 0.00975 0.00958 0.00958 0.01017 0.01008 0.01017 0.01017 0.01025 0.01033 0.01033 0.01033 0.01042 0.01042 0.01042 0.01042 0.01017 0.01017 0.01017 0.01017 0.0101 0.0003 2.9454 0.0096 0.0104 24

Strengthnorm [ksi] 43.432 43.118 43.951 42.308 43.467 42.360 41.608 39.478 42.512 41.606 42.216 43.519 43.737 43.731 43.380 41.494 39.634 38.400 40.322 37.763 37.794 38.643 39.186 38.683 41.35 2.1258 5.1412 37.76 43.95 24

43

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WT-MH-CTD MTM45-1/4581-35% RW QUARTZ "WARP TENSILE" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 135.91 132.43 135.93 132.95 122.96 135.14 109.73 107.95 122.10 108.37 120.84 89.80 133.21 104.16 124.44 NR 77.00 83.49 77.60 91.47 132.08 140.84 147.76 143.62 117.82 21.7508 18.4615 77.00 147.76 23

Modulus Poisson's Msi Ratio NR NR 4.22 0.09 3.71 0.14 3.57 0.08 3.68 0.13 NR NR 3.84 0.13 3.71 0.13 3.67 0.13 3.47 0.09 3.51 0.09 3.67 0.12 3.76 0.17 3.81 0.11 3.72 0.14 3.56 0.09 3.72 0.12 3.70 0.14 3.54 0.12 3.63 0.13 4.12 0.22 3.74 0.12 3.62 0.12 3.52 0.11 3.7041 0.1801 4.8628 3.4700 4.2200 22 0.1236 0.0303 24.5259 0.0800 0.2200 22

Avg. Specimen Thickn. [in] 0.1240 0.1220 0.1220 0.1220 0.1200 0.1200 0.1200 0.1200 0.1210 0.1220 0.1220 0.1220 0.1230 0.1220 0.1240 0.1220 0.1200 0.1240 0.1220 0.1220 0.1200 0.1220 0.1220 0.1260 0.1219 0.0015 1.2549 0.1200 0.1260 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01017 0.01017 0.01017 0.01000 0.01000 0.01000 0.01000 0.01008 0.01017 0.01017 0.01017 0.01025 0.01017 0.01033 0.01017 0.01000 0.01033 0.01017 0.01017 0.01000 0.01017 0.01017 0.01050 0.0102 0.0001 1.2549 0.0100 0.0105 24

Strengthnorm [ksi] 136.350 130.716 134.170 131.229 119.379 131.204 106.534 104.806 119.532 106.967 119.276 88.638 132.563 102.812 124.843 NR 74.757 83.760 76.595 90.286 128.233 139.017 145.847 146.409 116.26 21.8236 18.7718 74.76 146.41 23

44

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WT-MH-RTD MTM45-1/4581-35% RW QUARTZ "WARP TENSILE" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 98.77 100.24 91.83 88.25 94.15 93.93 102.59 95.44 99.61 99.68 99.92 91.43 103.13 102.72 101.91 92.32 94.03 100.33 97.24 4.5819 4.7121 88.25 103.13 18

Modulus Poisson's Msi Ratio 3.62 0.13 3.70 0.14 3.49 0.12 3.62 0.13 3.58 0.13 3.52 0.13 3.63 0.13 3.59 0.13 3.67 0.12 3.61 0.12 3.59 0.13 3.99 0.12 3.55 0.14 3.65 0.12 3.67 0.13 3.63 0.12 3.65 0.12 3.52 0.12 3.6267 0.1070 2.9516 3.4900 3.9900 18 0.1267 0.0069 5.4157 0.1200 0.1400 18

Avg. Specimen Thickn. [in] 0.1240 0.1240 0.1240 0.1220 0.1220 0.1230 0.1210 0.1210 0.1210 0.1230 0.1230 0.1230 0.1240 0.1230 0.1220 0.1240 0.1250 0.1260 0.1231 0.0014 1.1313 0.1210 0.1260 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01033 0.01033 0.01017 0.01017 0.01025 0.01008 0.01008 0.01008 0.01025 0.01025 0.01025 0.01033 0.01025 0.01017 0.01033 0.01042 0.01050 0.0103 0.0001 1.1313 0.0101 0.0105 18

Strengthnorm [ksi] 99.090 100.564 92.127 87.108 92.931 93.474 100.432 93.432 97.515 99.196 99.435 90.986 103.464 102.221 100.591 92.619 95.095 102.278 96.81 4.6735 4.8276 87.11 103.46 18

45

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WT-MH-ETW MTM45-1/4581-35% RW QUARTZ "WARP TENSILE" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 39.75 38.58 35.52 39.99 36.12 36.76 35.93 33.62 36.46 34.37 35.41 31.95 37.62 29.00 27.40 27.65 27.48 28.07 33.98 4.3403 12.7722 27.40 39.99 18

Modulus Poisson's Msi Ratio 3.70 0.11 3.66 0.12 3.55 0.10 3.72 0.12 3.74 0.12 3.75 0.12 3.63 0.12 4.25 0.14 4.23 0.14 3.58 0.11 3.68 0.13 3.84 0.12 3.93 0.12 3.96 0.12 3.65 0.12 3.60 0.13 3.79 0.13 3.55 0.11 3.7672 0.2077 5.5141 3.5500 4.2500 18 0.1211 0.0102 8.4437 0.1000 0.1400 18

Avg. Specimen Thickn. [in] 0.1240 0.1220 0.1220 0.1200 0.1210 0.1210 0.1230 0.1220 0.1220 0.1240 0.1230 0.1200 0.1230 0.1220 0.1250 0.1240 0.1250 0.1250 0.1227 0.0016 1.3115 0.1200 0.1250 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01017 0.01017 0.01000 0.01008 0.01008 0.01025 0.01017 0.01017 0.01033 0.01025 0.01000 0.01025 0.01017 0.01042 0.01033 0.01042 0.01042 0.0102 0.0001 1.3115 0.0100 0.0104 18

Strengthnorm [ksi] 39.879 38.081 35.060 38.825 35.360 35.987 35.756 33.185 35.988 34.481 35.238 31.019 37.437 28.625 27.710 27.739 27.791 28.388 33.70 4.1132 12.2065 27.71 39.88 18

46

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-WT-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "WARP TENSILE" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 36.27 34.30 32.80 36.98 37.06 34.87 36.68 37.37 29.30 30.53 28.70 31.37 30.54 30.54 28.93 30.41 25.64 25.69 25.03 26.53 28.08 26.38 26.29 27.74 30.75 4.1154 13.3829 25.03 37.37 24

Modulus Poisson's Msi Ratio NR NR NR NR NR NR NR NR NR NR NR 0.14 NR 0.10 NR NR NR NR NR NR NR NR NR NR 4.14 0.10 4.59 0.13 NR NR NR NR NR NR NR NR NR NR NR NR 3.89 0.12 NR NR NR NR NR NR 4.2067 0.3547 8.4326 3.8900 4.5900 3 0.1180 0.0179 15.1598 0.1000 0.1400 5

Avg. Specimen Thickn. [in] 0.1240 0.1240 0.1220 0.1220 0.1200 0.1210 0.1210 0.1200 0.1210 0.1220 0.1220 0.1220 0.1250 0.1240 0.1200 0.1240 0.1210 0.1230 0.1240 0.1230 0.1260 0.1240 0.1260 0.1230 0.1227 0.0018 1.4557 0.1200 0.1260 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01033 0.01017 0.01017 0.01000 0.01008 0.01008 0.01000 0.01008 0.01017 0.01017 0.01017 0.01042 0.01033 0.01000 0.01033 0.01008 0.01025 0.01033 0.01025 0.01050 0.01033 0.01050 0.01025 0.0102 0.0001 1.4557 0.0100 0.0105 24

Strengthnorm [ksi] 36.387 34.411 32.375 36.501 35.981 34.136 35.908 36.282 28.684 30.135 28.328 30.964 30.886 30.639 28.087 30.508 25.101 25.565 25.111 26.401 28.625 26.465 26.800 27.605 30.50 3.9064 12.8099 25.10 36.50 24

47

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FT-MH-CTD MTM45-1/4581-35% RW QUARTZ "FILL TENSILE" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 84.78 84.20 75.89 72.00 124.83 128.17 116.96 132.35 126.48 132.15 133.63 114.69 98.94 123.19 105.51 89.02 88.06 72.04 66.69 78.87 92.85 98.59 91.23 84.78 100.66 22.0609 21.9157 66.69 133.63 24

Modulus Poisson's Msi Ratio 3.72 0.10 3.55 0.11 3.49 0.12 3.91 0.20 2.80 0.05 2.77 0.08 3.59 0.13 3.43 0.12 3.66 0.15 3.73 0.15 3.76 0.19 3.41 0.07 4.03 0.13 3.68 0.14 3.49 0.12 3.45 0.08 3.53 0.12 3.64 0.13 3.48 0.12 3.64 0.13 3.44 NR 3.27 0.09 3.40 0.11 3.56 0.15 3.5179 0.2819 8.0138 2.7700 4.0300 24 0.1213 0.0349 28.8053 0.0500 0.2000 23

Avg. Specimen Thickn. [in] 0.1210 0.1230 0.1240 0.1230 0.1230 0.1270 0.1240 0.1260 0.1230 0.1210 0.1220 0.1240 0.1230 0.1210 0.1230 0.1230 0.1230 0.1210 0.1260 0.1210 0.1240 0.1250 0.1270 0.1260 0.1235 0.0019 1.5289 0.1210 0.1270 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01008 0.01025 0.01033 0.01025 0.01025 0.01058 0.01033 0.01050 0.01025 0.01008 0.01017 0.01033 0.01025 0.01008 0.01025 0.01025 0.01025 0.01008 0.01050 0.01008 0.01033 0.01042 0.01058 0.01050 0.0103 0.0002 1.5289 0.0101 0.0106 24

Strengthnorm [ksi] 82.997 83.791 76.136 71.650 124.224 131.696 117.339 134.920 125.866 129.370 131.900 115.061 98.460 120.599 104.998 88.588 87.633 70.525 67.985 77.211 93.150 99.707 93.740 86.426 100.58 22.0896 21.9618 67.98 134.92 24

48

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FT-MH-RTD MTM45-1/4581-35% RW QUARTZ "FILL TENSILE" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 83.25 79.84 92.45 100.19 96.13 101.34 96.28 96.01 99.11 95.09 88.87 92.32 87.97 88.20 87.81 84.44 79.82 80.64 90.54 7.0500 7.7864 79.82 101.34 18

Modulus Poisson's Msi Ratio 3.50 0.12 3.57 0.13 3.70 0.12 3.48 0.12 3.41 0.12 3.51 0.12 3.59 0.12 3.61 0.12 3.58 0.13 3.44 0.12 3.49 0.12 3.51 0.13 3.49 0.12 3.51 0.12 3.48 0.12 3.37 0.12 3.33 0.12 3.37 0.11 3.4967 0.0930 2.6594 3.3300 3.7000 18 0.1211 0.0047 3.8923 0.1100 0.1300 18

Avg. Specimen Thickn. [in] 0.1240 0.1230 0.1240 0.1230 0.1230 0.1230 0.1220 0.1230 0.1210 0.1240 0.1240 0.1240 0.1220 0.1200 0.1210 0.1270 0.1270 0.1260 0.1234 0.0019 1.5512 0.1200 0.1270 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01025 0.01033 0.01025 0.01025 0.01025 0.01017 0.01025 0.01008 0.01033 0.01033 0.01033 0.01017 0.01000 0.01008 0.01058 0.01058 0.01050 0.0103 0.0002 1.5512 0.0100 0.0106 18

Strengthnorm [ksi] 83.519 79.452 92.749 99.704 95.663 100.848 95.034 95.544 97.025 95.398 89.158 92.619 86.831 85.631 85.963 86.763 82.016 82.206 90.34 6.5313 7.2296 79.45 100.85 18

49

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FT-MH-ETW MTM45-1/4581-35% RW QUARTZ "FILL TENSILE" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21

ACG Batch # D D D D A A A A B B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 2 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 33.15 31.22 29.59 26.78 31.47 32.12 31.34 35.03 23.23 24.37 24.23 24.57 26.87 27.20 27.37 25.58 25.45 22.23 21.03 23.92 20.58 27.02 4.1250 15.2689 20.58 35.03 21

Modulus Poisson's Msi Ratio 3.40 0.11 3.69 0.10 3.47 0.11 3.78 0.12 3.29 0.11 3.69 0.11 NR NR 3.69 0.12 3.46 0.10 4.33 0.12 3.63 0.11 3.50 0.11 3.42 0.11 3.38 0.11 3.34 0.11 3.40 0.10 3.76 0.11 3.93 0.12 3.31 0.12 3.84 0.11 3.40 0.12 3.5855 0.2589 7.2206 3.2900 4.3300 20 0.1115 0.0067 6.0163 0.1000 0.1200 20

Avg. Specimen Thickn. [in] 0.1230 0.1230 0.1200 0.1180 0.1240 0.1200 0.1240 0.1230 0.1230 0.1220 0.1230 0.1220 0.1240 0.1240 0.1240 0.1240 0.1240 0.1230 0.1280 0.1270 0.1270 0.1233 0.0023 1.8725 0.1180 0.1280 21

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01025 0.01025 0.01000 0.00983 0.01033 0.01000 0.01033 0.01025 0.01025 0.01017 0.01025 0.01017 0.01033 0.01033 0.01033 0.01033 0.01033 0.01025 0.01067 0.01058 0.01058 0.0103 0.0002 1.8725 0.0098 0.0107 21

Strengthnorm [ksi] 32.989 31.068 28.728 25.567 31.572 31.184 31.441 34.860 23.117 24.055 24.112 24.252 26.957 27.288 27.459 25.663 25.532 22.122 21.779 24.578 21.146 26.93 3.9518 14.6760 21.15 34.86 21

50

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FT-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "FILL TENSILE" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # D D D D A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 26.63 30.04 28.61 28.18 31.32 32.78 31.09 30.14 23.06 23.82 23.40 23.43 24.11 24.02 24.91 24.11 21.47 21.53 25.20 20.51 20.33 21.47 21.43 19.35 25.04 3.9094 15.6131 19.35 32.78 24

Modulus Poisson's Msi Ratio NR NR NR NR NR NR NR NR NR 0.13 NR NR NR 0.16 NR 0.16 NR NR NR NR NR NR NR NR 4.51 0.14 NR NR NR NR 4.24 0.11 NR NR NR NR 3.49 0.11 NR NR NR NR 4.75 0.15 NR NR 4.19 0.11 4.2360 0.4738 11.1849 3.4900 4.7500 5 0.1338 0.0220 16.4474 0.1100 0.1600 8

Avg. Specimen Thickn. [in] 0.1230 0.1220 0.1230 0.1220 0.1230 0.1220 0.1220 0.1200 0.1230 0.1220 0.1230 0.1230 0.1230 0.1240 0.1250 0.1240 0.1240 0.1240 0.1240 0.1240 0.1280 0.1260 0.1260 0.1270 0.1236 0.0018 1.4472 0.1200 0.1280 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01025 0.01017 0.01025 0.01017 0.01025 0.01017 0.01017 0.01000 0.01025 0.01017 0.01025 0.01025 0.01025 0.01033 0.01042 0.01033 0.01033 0.01033 0.01033 0.01033 0.01067 0.01050 0.01050 0.01058 0.0103 0.0001 1.4472 0.0100 0.0107 24

Strengthnorm [ksi] 26.501 29.651 28.471 27.815 31.168 32.356 30.688 29.262 22.948 23.512 23.286 23.316 23.993 24.098 25.192 24.188 21.539 21.600 25.282 20.576 21.054 21.887 21.846 19.882 25.00 3.6465 14.5833 19.88 32.36 24

51

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNT1-MH-CTD MTM45-1/4581-35% RW QUARTZ "UNNOTCHED TENSILE" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 106.94 99.46 102.56 100.97 83.07 85.57 87.37 87.50 98.91 98.09 100.83 94.47 95.71 97.93 93.66 99.53 78.97 91.05 89.09 NR 98.82 94.68 86.01 79.87 93.52 7.6078 8.1345 78.97 106.94 23

Modulus Poisson's Msi Ratio 2.95 0.23 3.16 0.30 3.02 0.28 3.09 0.28 2.42 0.39 2.49 0.30 2.42 0.30 3.07 0.26 3.43 NR 3.21 0.31 3.03 0.28 2.94 0.28 3.47 NR 2.85 0.21 2.92 0.23 2.99 0.29 3.09 0.27 2.94 0.27 3.05 0.27 3.04 0.27 3.07 0.29 2.95 0.25 2.93 0.25 3.01 0.26 2.9808 0.2534 8.5019 2.4200 3.4700 24 0.2759 0.0358 12.9795 0.2100 0.3900 22

Avg. Specimen Thickn. [in] 0.1190 0.1180 0.1190 0.1190 0.1220 0.1210 0.1210 0.1180 0.1240 0.1240 0.1240 0.1240 0.1230 0.1240 0.1240 0.1240 0.1260 0.1260 0.1260 0.1260 0.1250 0.1260 0.1260 0.1270 0.1232 0.0029 2.3171 0.1180 0.1270 24

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00992 0.00983 0.00992 0.00992 0.01017 0.01008 0.01008 0.00983 0.01033 0.01033 0.01033 0.01033 0.01025 0.01033 0.01033 0.01033 0.01050 0.01050 0.01050 0.01050 0.01042 0.01050 0.01050 0.01058 0.0103 0.0002 2.3171 0.0098 0.0106 24

Strengthnorm [ksi] 102.960 94.954 98.743 97.212 81.995 83.770 85.532 83.536 99.230 98.407 101.156 94.776 95.245 98.247 93.963 99.852 80.503 92.818 90.820 NR 99.939 96.518 87.680 82.067 93.04 7.0481 7.5753 80.50 102.96 23

52

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNT1-MH-RTD MTM45-1/4581-35% RW QUARTZ "UNNOTCHED TENSILE" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 79.22 80.32 77.84 73.77 75.55 74.92 78.96 81.18 79.24 74.98 77.64 77.77 73.83 72.75 74.02 76.61 75.00 75.36 76.61 2.4972 3.2597 72.75 81.18 18

Modulus Poisson's Msi Ratio 2.91 0.30 2.93 0.30 2.96 0.30 2.85 0.33 2.91 0.33 2.95 0.32 2.86 0.29 2.94 .2+9 2.93 0.29 2.92 0.29 2.86 0.28 2.91 0.28 2.90 0.28 2.87 0.28 2.92 0.26 2.93 0.27 2.90 0.29 2.98 0.30 2.9128 0.0356 1.2227 2.8500 2.9800 18 0.2935 0.0193 6.5908 0.2600 0.3300 17

Avg. Specimen Thickn. [in] 0.1180 0.1190 0.1190 0.1220 0.1220 0.1220 0.1230 0.1240 0.1240 0.1240 0.1240 0.1240 0.1260 0.1260 0.1260 0.1260 0.1260 0.1260 0.1234 0.0026 2.1196 0.1180 0.1260 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00983 0.00992 0.00992 0.01017 0.01017 0.01017 0.01025 0.01033 0.01033 0.01033 0.01033 0.01033 0.01050 0.01050 0.01050 0.01050 0.01050 0.01050 0.0103 0.0002 2.1196 0.0098 0.0105 18

Strengthnorm [ksi] 75.631 77.331 74.943 72.815 74.572 73.950 78.577 81.443 79.496 75.223 77.891 78.022 75.264 74.163 75.457 78.098 76.456 76.823 76.45 2.1959 2.8722 72.82 81.44 18

53

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-UNT1-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "UNNOTCHED TENSILE" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8

ACG Batch # A A A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 26.22 27.94 29.25 28.80 26.17 28.50 28.83 27.36 27.88 1.1931 4.2787 26.17 29.25 8

Modulus Poisson's Msi Ratio NR NR NR NR NR NR NR NR NR NR NR NR 2.89 0.41 NR NR 2.8900 NA NA 2.8900 2.8900 1 0.4100 NA NA 0.4100 0.4100 1

Avg. Specimen Thickn. [in] 0.1150 0.1180 0.1180 0.1180 0.1210 0.1220 0.1210 0.1220 0.1194 0.0025 2.0972 0.1150 0.1220 8

# Plies in Laminate 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00958 0.00983 0.00983 0.00983 0.01008 0.01017 0.01008 0.01017 0.0099 0.0002 2.0972 0.0096 0.0102 8

Strengthnorm [ksi] 24.396 26.674 27.925 27.495 25.619 28.131 28.224 27.006 26.93 1.3436 4.9884 24.40 28.22 8

54

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT1-MH-CTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 1" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

ACG Batch # A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 51.22 52.68 50.63 52.28 54.06 52.29 52.68 50.96 52.27 50.53 48.92 49.97 49.70 48.20 49.27 49.12 50.92 1.6670 3.2735 48.20 54.06 16

Load (lbs) 9234 9189 9250 9490 9897 9420 9748 9425 9670 9346 9160 9389 9304 9113 9157 9227 9376 227.573 2.4271 9113 9897 16

Avg Width (in) 1.496 1.497 1.497 1.497 1.495 1.495 1.497 1.496 1.496 1.496 1.496 1.496 1.495 1.496 1.494 1.496 1.496 0.0009 0.0571 1.494 1.497 16

Avg Thickness (in) 0.120 0.117 0.122 0.121 0.122 0.120 0.124 0.124 0.124 0.124 0.125 0.126 0.125 0.126 0.124 0.126 0.123 0.0026 2.0944 0.117 0.126 16

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.00975 0.01017 0.01008 0.01017 0.01000 0.01033 0.01033 0.01033 0.01033 0.01042 0.01050 0.01042 0.01050 0.01033 0.01050 0.0103 0.0002 2.0944 0.0098 0.0105 16

Strengthnorm [ksi] 49.728 49.867 49.975 51.180 53.360 50.767 52.850 51.125 52.439 50.694 49.474 50.940 50.263 49.136 49.429 50.074 50.71 1.2519 2.4690 49.14 53.36 16

55

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT1-MH-RTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 1" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 41.17 41.23 41.08 41.56 42.21 41.06 42.48 42.40 42.80 42.16 42.33 42.28 39.22 39.98 38.45 39.17 39.29 39.05 41.00 1.4307 3.4900 38.45 42.80 18

Load (lbs) 7499 7459 7412 7423 7513 7450 7861 7816 7863 7884 7742 7774 7344 7430 7219 7326 7358 7338 7540 219.3389 2.9092 7219 7884 18

Avg Width (in) 1.497 1.497 1.498 1.497 1.497 1.496 1.497 1.496 1.496 1.498 1.498 1.497 1.496 1.494 1.495 1.494 1.496 1.496 1.496 0.0012 0.0799 1.494 1.498 18

Avg Thickness (in) 0.122 0.121 0.120 0.119 0.119 0.121 0.124 0.123 0.123 0.125 0.122 0.123 0.125 0.124 0.126 0.125 0.125 0.126 0.123 0.0023 1.8394 0.119 0.126 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.01008 0.01000 0.00992 0.00992 0.01008 0.01033 0.01025 0.01025 0.01042 0.01017 0.01025 0.01042 0.01033 0.01050 0.01042 0.01042 0.01050 0.0102 0.0002 1.8394 0.0099 0.0105 18

Strengthnorm [ksi] 40.637 40.363 39.883 40.013 40.639 40.196 42.617 42.194 42.592 42.638 41.782 42.075 39.664 40.109 39.197 39.614 39.735 39.808 40.76 1.1964 2.9348 39.20 42.64 18

56

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT1-MH-ETW MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 1" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 14.15 14.50 14.24 14.28 14.06 14.37 14.27 0.1564 1.0964 14.06 14.50 6

Load (lbs) 2588 2613 2608 2584 2552 2543 2581 28.6193 1.1087 2543 2613 6

Avg Width (in) 1.498 1.496 1.496 1.497 1.497 1.498 1.4970 0.0009 0.0597 1.496 1.498 6

Avg Thickness (in) 0.122 0.120 0.122 0.121 0.121 0.118 0.121 0.0015 1.2477 0.118 0.122 6

# Plies in Laminate 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01017 0.01000 0.01017 0.01008 0.01008 0.00983 0.0101 0.0001 1.2477 0.0098 0.0102 6

Strengthnorm [ksi] 13.967 14.078 14.056 13.980 13.764 13.719 13.93 0.1506 1.0813 13.72 14.08 6

57

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT1-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 1" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 13.63 13.31 12.83 13.32 12.88 12.93 11.78 12.48 11.63 11.95 12.31 12.15 12.06 11.74 11.99 11.26 11.07 11.40 12.26 0.7509 6.1240 11.07 13.63 18

Load (lbs) 2449 2408 2350 2377 2337 2323 2179 2197 2159 2204 2278 2256 2235 2177 2247 2123 2058 2155 2251 105.7834 4.7001 2058 2449 18

Avg Width (in) 1.496 1.498 1.496 1.496 1.496 1.496 1.496 1.496 1.496 1.497 1.497 1.497 1.495 1.496 1.496 1.496 1.495 1.496 1.496 0.0007 0.0473 1.495 1.498 18

Avg Thickness (in) 0.120 0.121 0.122 0.119 0.121 0.120 0.124 0.118 0.124 0.123 0.124 0.124 0.124 0.124 0.125 0.126 0.124 0.126 0.1227 0.0024 1.9324 0.1180 0.1260 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.01008 0.01017 0.00992 0.01008 0.01000 0.01033 0.00983 0.01033 0.01025 0.01033 0.01033 0.01033 0.01033 0.01042 0.01050 0.01033 0.01050 0.0102 0.0002 1.9324 0.0098 0.0105 18

Strengthnorm [ksi] 13.233 13.030 12.664 12.824 12.609 12.553 11.818 11.915 11.668 11.892 12.350 12.189 12.099 11.778 12.126 11.479 11.106 11.621 12.16 0.5690 4.6779 11.11 13.23 18

58

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT2-MH-CTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 2" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 44.80 44.22 43.48 44.51 44.88 45.42 44.55 0.6609 1.4834 43.48 45.42 6

Load (lbs) 10258 10245 10070 10065 10292 10389 10220 128.3268 1.2557 10065 10389 6

Avg Width (in) 1.495 1.497 1.497 1.496 1.497 1.497 1.4965 0.0008 0.0559 1.495 1.497 6

Avg Thickness (in) 0.153 0.155 0.155 0.151 0.153 0.153 0.153 0.0015 0.9819 0.151 0.155 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01020 0.01033 0.01033 0.01007 0.01020 0.01020 0.0102 0.0001 0.9819 0.0101 0.0103 6

Strengthnorm [ksi] 44.365 44.363 43.621 43.502 44.444 44.979 44.21 0.5555 1.2564 43.50 44.98 6

59

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT2-MH-RTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 2" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 36.43 35.56 36.90 36.35 36.25 37.37 36.48 0.6144 1.6842 35.56 37.37 6

Load (lbs) 8445 8268 8506 8308 8288 8389 8367 95.301 1.1390 8268 8506 6

Avg Width (in) 1.494 1.495 1.498 1.496 1.497 1.496 1.496 0.0014 0.0945 1.494 1.498 6

Avg Thickness (in) 0.155 0.156 0.154 0.153 0.153 0.150 0.154 0.0021 1.3509 0.150 0.156 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01040 0.01027 0.01020 0.01020 0.01000 0.0102 0.0001 1.3509 0.0100 0.0104 6

Strengthnorm [ksi] 36.548 35.905 36.781 35.997 35.898 36.282 36.24 0.3679 1.0152 35.90 36.78 6

60

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT2-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 2" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 13.04 12.89 12.48 13.25 12.84 12.78 12.88 0.2585 2.0073 12.48 13.25 6

Load (lbs) 3002 2968 2860 3006 2905 2903 2941 59.9589 2.0390 2860 3006 6

Avg Width (in) 1.496 1.496 1.497 1.496 1.496 1.498 1.4965 0.0008 0.0559 1.496 1.498 6

Avg Thickness (in) 0.154 0.154 0.153 0.152 0.151 0.152 0.153 0.0012 0.7933 0.151 0.154 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01027 0.01027 0.01020 0.01013 0.01007 0.01013 0.0102 0.0001 0.7933 0.0101 0.0103 6

Strengthnorm [ksi] 12.998 12.848 12.359 13.036 12.549 12.573 12.73 0.2735 2.1492 12.36 13.04 6

61

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT3-MH-CTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 3" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 63.89 65.87 63.42 61.25 63.72 64.62 63.80 1.5244 2.3895 61.25 65.87 6

Load (lbs) 14323 14871 14532 14154 14570 14585 14506 245.614 1.6932 14154 14871 6

Avg Width (in) 1.498 1.497 1.496 1.497 1.497 1.497 1.497 0.0006 0.0422 1.496 1.498 6

Avg Thickness (in) 0.150 0.151 0.153 0.154 0.153 0.151 0.152 0.0015 1.0192 0.150 0.154 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.01007 0.01020 0.01027 0.01020 0.01007 0.0101 0.0001 1.0192 0.0100 0.0103 6

Strengthnorm [ksi] 62.029 64.378 62.804 61.052 63.101 63.156 62.75 1.1265 1.7951 61.05 64.38 6

62

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT3-MH-RTD MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 3" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 47.57 48.81 47.58 45.64 46.52 44.86 46.83 1.4439 3.0832 44.86 48.81 6

Load (lbs) 10883 11081 11018 10595 10577 10337 10749 291.0613 2.7079 10337 11081 6

Avg Width (in) 1.498 1.498 1.496 1.496 1.496 1.497 1.4968 0.0010 0.0657 1.496 1.498 6

Avg Thickness (in) 0.153 0.152 0.155 0.155 0.152 0.154 0.154 0.0014 0.8980 0.152 0.155 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01020 0.01013 0.01033 0.01033 0.01013 0.01027 0.0102 0.0001 0.8980 0.0101 0.0103 6

Strengthnorm [ksi] 47.108 48.020 47.734 45.788 45.767 44.715 46.52 1.2986 2.7914 44.71 48.02 6

63

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-OHT3-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "OPEN HOLE TENSILE 3" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 15.80 16.42 15.83 15.80 15.33 15.58 15.79 0.3618 2.2906 15.33 16.42 6

Load (lbs) 3649 3734 3599 3568 3541 3516 3601 79.8885 2.2184 3516 3734 6

Avg Width (in) 1.496 1.496 1.496 1.497 1.496 1.497 1.496 0.0005 0.0345 1.496 1.497 6

Avg Thickness (in) 0.154 0.152 0.152 0.151 0.154 0.151 0.152 0.0014 0.8969 0.151 0.154 6

# Plies in Laminate 15 15 15 15 15 15 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01027 0.01013 0.01013 0.01007 0.01027 0.01007 0.0102 0.0001 0.8969 0.0101 0.0103 6

Strengthnorm [ksi] 15.749 16.154 15.574 15.442 15.280 15.227 15.57 0.3439 2.2084 15.23 16.15 6

64

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FHT1-MH-CTD MTM45-1/4581-35% RW QUARTZ "FILLED HOLE TENSILE 1" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 53.29 54.84 55.08 53.81 53.89 55.42 54.19 53.75 53.77 54.45 54.67 56.04 52.14 51.96 52.34 51.16 51.84 51.88 53.58 1.4121 2.6353 51.16 56.04 18

Load (lbs) 9573 9921 9951 9638 9683 9964 10056 9912 9987 10036 10094 10303 9636 9659 9737 9584 9746 9656 9841 210.734 2.1414 9573 10303 18

Avg Width (in) 1.496 1.497 1.500 1.496 1.496 1.497 1.496 1.496 1.498 1.496 1.498 1.497 1.495 1.499 1.495 1.496 1.497 1.496 1.497 0.0013 0.0882 1.495 1.500 18

Avg Thickness (in) 0.120 0.121 0.120 0.120 0.120 0.120 0.124 0.123 0.124 0.123 0.123 0.123 0.124 0.124 0.124 0.125 0.126 0.124 0.123 0.0020 1.6063 0.120 0.126 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.01008 0.01000 0.01000 0.01000 0.01000 0.01033 0.01025 0.01033 0.01025 0.01025 0.01025 0.01033 0.01033 0.01033 0.01042 0.01050 0.01033 0.0102 0.0002 1.6063 0.0100 0.0105 18

Strengthnorm [ksi] 51.738 53.686 53.476 52.243 52.320 53.806 54.365 53.489 53.944 54.186 54.405 55.768 52.309 52.128 52.509 51.739 52.847 52.048 53.17 1.1247 2.1155 51.74 55.77 18

65

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-FHT1-MH-RTD MTM45-1/4581-35% RW QUARTZ "FILLED HOLE TENSILE 1" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6

ACG Batch # A A A A A A

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 46.06 45.87 45.12 44.44 44.86 44.91 45.21 0.6279 1.3890 44.44 46.06 6

Load (lbs) 8252 8299 8203 8066 8066 8045 8155 109.9007 1.3476 8045 8299 6

Avg Width (in) 1.497 1.497 1.499 1.497 1.497 1.497 1.4973 0.0008 0.0545 1.497 1.499 6

Avg Thickness (in) 0.120 0.121 0.121 0.121 0.120 0.120 0.121 0.0005 0.4545 0.120 0.121 6

# Plies in Laminate 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01000 0.01008 0.01008 0.01008 0.01000 0.01000 0.0100 0.0000 0.4545 0.0100 0.0101 6

Strengthnorm [ksi] 44.718 44.905 44.171 43.505 43.553 43.602 44.08 0.6217 1.4106 43.51 44.91 6

66

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-IPS-MH-CTD MTM45-1/4581-35% RW QUARTZ "IN-PLANE SHEAR Strength @ 5% Shear Strain" Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 25.18 25.03 25.28 25.66 25.91 25.78 26.08 26.12 23.88 23.64 25.76 23.37 23.59 22.74 23.14 22.48 24.27 23.77 23.70 24.11 25.08 25.72 25.23 26.16 24.65 1.1650 4.7255 22.48 26.16 24

Modulus Poisson's Msi Ratio 0.76 0.499 0.73 0.450 0.75 0.449 0.75 0.441 0.71 0.444 0.76 0.465 NR NR 0.73 0.478 0.70 0.416 0.71 0.518 0.77 0.496 0.71 0.459 0.73 0.469 0.69 0.445 0.68 0.424 0.70 0.421 0.74 0.494 NR NR 0.75 0.471 0.72 0.444 0.79 0.455 0.81 0.397 NR NR NR NR 0.7345 0.0336 4.5793 0.6800 0.8100 20 0.4568 0.0306 6.6906 0.3970 0.5180 20

Avg. Specimen Thickn. [in] 0.0820 0.0810 0.0820 0.0820 0.0820 0.0820 0.0810 0.0820 0.0840 0.0840 0.0800 0.0850 0.0810 0.0830 0.0830 0.0830 0.0820 0.0820 0.0810 0.0820 0.0790 0.0820 0.0830 0.0830 0.0821 0.0013 1.5780 0.0790 0.0850 24

# Plies in Laminate 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01025 0.01013 0.01025 0.01025 0.01025 0.01025 0.01013 0.01025 0.01050 0.01050 0.01000 0.01063 0.01013 0.01038 0.01038 0.01038 0.01025 0.01025 0.01013 0.01025 0.00988 0.01025 0.01038 0.01038 0.0103 0.0002 1.5780 0.0099 0.0106 24

Strengthnorm [ksi] 25.058 24.605 25.157 25.535 25.784 25.655 25.637 25.993 24.344 24.099 25.010 24.107 23.189 22.906 23.308 22.644 24.152 23.655 23.297 23.993 24.045 25.595 25.414 26.350 24.56 1.0665 4.3419 22.64 26.35 24

67

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-IPS-MH-RTD MTM45-1/4581-35% RW QUARTZ "IN-PLANE SHEAR Strength @ 5% Shear Strain" Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 19.05 18.90 19.35 18.53 18.44 19.55 19.15 18.42 18.96 18.11 17.67 17.93 20.60 20.08 19.59 21.03 21.03 22.70 19.39 1.2891 6.6471 17.67 22.70 18

Modulus Poisson's Msi Ratio 0.60 0.539 0.58 0.519 0.58 0.518 0.58 0.542 0.58 0.538 0.59 0.537 0.60 0.529 0.59 0.504 0.59 0.521 0.56 0.529 0.54 0.535 0.52 0.516 0.59 0.495 0.60 0.506 0.58 0.509 0.61 0.496 0.60 0.496 0.63 0.488 0.5844 0.0250 4.2815 0.5200 0.6300 18 0.5176 0.0174 3.3588 0.4880 0.5420 18

Avg. Specimen Thickn. [in] 0.0820 0.0820 0.0810 0.0810 0.0830 0.0820 0.0820 0.0840 0.0830 0.0830 0.0830 0.0830 0.0810 0.0820 0.0840 0.0830 0.0830 0.0820 0.0824 0.0009 1.1181 0.0810 0.0840 18

# Plies in Laminate 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01025 0.01025 0.01013 0.01013 0.01038 0.01025 0.01025 0.01050 0.01038 0.01038 0.01038 0.01038 0.01013 0.01025 0.01050 0.01038 0.01038 0.01025 0.0103 0.0001 1.1181 0.0101 0.0105 18

Strengthnorm [ksi] 18.958 18.808 19.021 18.215 18.574 19.455 19.057 18.778 19.098 18.242 17.799 18.061 20.250 19.983 19.970 21.183 21.183 22.590 19.40 1.2601 6.4951 17.80 22.59 18

68

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-IPS-MH-ETW MTM45-1/4581-35% RW QUARTZ "IN-PLANE SHEAR Strength @ 5% Shear Strain" Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19

ACG Batch # A A A A A A B B B B B B C C C C B C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 2 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 12.66 12.61 12.76 13.46 14.02 13.62 13.84 11.58 10.56 11.93 10.80 11.07 10.90 12.45 12.65 12.35 12.74 12.93 12.33 12.38 1.0239 8.2695 10.56 14.02 19

Modulus Poisson's Msi Ratio 0.39 0.662 0.38 0.667 0.41 0.653 0.48 0.820 0.42 0.612 0.42 0.624 0.43 0.645 0.38 0.632 0.39 0.644 0.40 0.655 0.40 0.608 0.40 0.643 0.40 0.642 0.39 0.652 0.44 0.632 0.41 0.630 0.46 0.673 0.43 0.577 0.42 0.658 0.41 0.026 6.4064 0 0 19 0.649 0.0474 7.2988 0.577 0.820 19

Avg Thickness (in) 0.081 0.082 0.082 0.082 0.080 0.082 0.078 0.083 0.084 0.081 0.083 0.083 0.082 0.082 0.081 0.078 0.083 0.081 0.083 0.082 0.0016 1.9673 0.078 0.084 19

# Plies in Laminate 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01013 0.01025 0.01025 0.01025 0.01000 0.01025 0.00975 0.01038 0.01050 0.01013 0.01038 0.01038 0.01025 0.01025 0.01013 0.00975 0.01038 0.01013 0.01038 0.0102 0.0002 1.9673 0.0098 0.0105 19

Strengthnorm [ksi] 12.445 12.549 12.698 13.395 13.612 13.554 13.101 11.664 10.765 11.727 10.879 11.151 10.847 12.390 12.435 11.691 12.833 12.710 12.420 12.26 0.9050 7.3840 10.77 13.61 19

69

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-IPS-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "IN-PLANE SHEAR Strength @ 5% Shear Strain" Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 13 14 15 17 18 19 20 21 22 23 24

ACG Batch # A A A A A A A A B B B B B B C C C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 10.15 10.37 10.20 10.50 10.68 10.98 10.55 11.06 9.51 9.47 9.31 8.84 8.74 8.24 9.37 9.97 9.68 10.06 10.69 10.70 10.93 10.60 10.03 0.7869 7.8480 8.24 11.06 22

Modulus Poisson's Msi Ratio NR NR 0.32 0.778 0.34 0.799 0.35 0.848 NR NR 0.40 1.006 0.37 0.812 0.37 1.048 0.34 0.747 0.36 0.921 0.35 0.819 0.32 0.939 0.31 0.817 0.35 0.878 NR NR 0.34 0.788 NR NR 0.32 0.757 0.34 0.905 0.34 0.661 0.37 0.942 0.38 0.823 0.3483 0.0236 6.7686 0.3100 0.4000 18 0.8493 0.0969 11.4082 0.6610 1.0480 18

Avg. Specimen Thickn. [in] 0.0810 0.0820 0.0820 0.0810 0.0820 0.0820 0.0830 0.0820 0.0830 0.0840 0.0830 0.0840 0.0840 0.0830 0.0810 0.0810 0.0820 0.0820 0.0830 0.0830 0.0830 0.0830 0.0825 0.0010 1.1673 0.0810 0.0840 22

# Plies in Laminate 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01013 0.01025 0.01025 0.01013 0.01025 0.01025 0.01038 0.01025 0.01038 0.01050 0.01038 0.01050 0.01050 0.01038 0.01013 0.01013 0.01025 0.01025 0.01038 0.01038 0.01038 0.01038 0.0103 0.0001 1.1673 0.0101 0.0105 22

Strengthnorm [ksi] 9.978 10.320 10.150 10.322 10.628 10.927 10.627 11.006 9.579 9.654 9.378 9.012 8.910 8.300 9.211 9.801 9.633 10.011 10.768 10.778 11.010 10.677 10.03 0.7583 7.5600 8.30 11.01 22

70

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS1-MH-CTD MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (QSBS)" 90° SPECIMENS FROM "UNT1" LAMINATES Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 12.79 12.87 12.01 13.81 12.96 13.73 12.72 12.38 12.71 11.93 12.81 12.48 11.32 11.31 11.37 11.38 11.59 11.06 12.29 0.8360 6.8022 11.06 13.81 18

Load (lbs) 500 510 472 553 520 549 518 505 510 495 529 515 477 474 474 483 491 462 502 26.181 5.2148 462 553 18

Avg Width (in) 0.252 0.254 0.252 0.252 0.251 0.251 0.249 0.250 0.249 0.251 0.251 0.252 0.252 0.251 0.252 0.253 0.252 0.251 0.251 0.0012 0.4946 0.249 0.254 18

Avg Thickness (in) 0.117 0.117 0.117 0.119 0.120 0.119 0.122 0.122 0.121 0.124 0.123 0.123 0.126 0.125 0.124 0.126 0.126 0.125 0.122 0.0032 2.6223 0.117 0.126 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00975 0.00975 0.00975 0.00992 0.01000 0.00992 0.01017 0.01017 0.01008 0.01033 0.01025 0.01025 0.01050 0.01042 0.01033 0.01050 0.01050 0.01042 0.0102 0.0003 2.6223 0.0098 0.0105 18

Strengthnorm [ksi] 12.107 12.183 11.369 13.296 12.583 13.219 12.555 12.220 12.443 11.969 12.748 12.419 11.540 11.438 11.407 11.601 11.815 11.185 12.12 0.6292 5.1928 11.19 13.30 18

71

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS1-MH-RTD MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (QSBS)" 90° SPECIMENS FROM "UNT1" LAMINATES Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 10.12 10.35 10.06 10.34 10.34 10.54 10.53 10.45 10.47 10.32 10.23 10.33 9.80 9.95 9.96 9.74 10.00 10.09 10.20 0.2454 2.4054 9.74 10.54 18

Load (lbs) 396 406 397 419 415 430 426 425 428 427 421 432 408 415 418 412 426 422 418 10.702 2.5606 396 432 18

Avg Width (in) 0.252 0.254 0.253 0.251 0.252 0.252 0.250 0.250 0.250 0.252 0.252 0.252 0.251 0.251 0.251 0.251 0.252 0.252 0.252 0.0010 0.4141 0.250 0.254 18

Avg Thickness (in) 0.116 0.116 0.117 0.121 0.120 0.121 0.121 0.122 0.123 0.123 0.122 0.124 0.124 0.124 0.126 0.126 0.127 0.124 0.122 0.0032 2.6581 0.116 0.127 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00967 0.00967 0.00975 0.01008 0.01000 0.01008 0.01008 0.01017 0.01025 0.01025 0.01017 0.01033 0.01033 0.01033 0.01050 0.01050 0.01058 0.01033 0.0102 0.0003 2.6581 0.0097 0.0106 18

Strengthnorm [ksi] 9.498 9.714 9.523 10.122 10.039 10.318 10.308 10.315 10.419 10.270 10.098 10.363 9.832 9.982 10.153 9.929 10.275 10.123 10.07 0.2787 2.7678 9.50 10.42 18

72

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS1-MH-ETW MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (QSBS)" 90° SPECIMENS FROM "UNT1" LAMINATES Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 5.37 5.61 5.32 5.98 5.30 5.86 4.67 4.68 4.71 4.64 4.86 4.57 4.57 4.84 4.69 4.69 4.61 4.90 4.99 0.4598 9.2102 4.57 5.98 18

Load (lbs) 203 212 209 242 213 237 189 193 194 194 201 188 190 202 196 198 195 207 204 15.147 7.4434 188 242 18

Avg Width (in) 0.252 0.252 0.253 0.252 0.252 0.252 0.250 0.248 0.251 0.252 0.252 0.253 0.251 0.252 0.252 0.252 0.252 0.251 0.252 0.0011 0.4550 0.248 0.253 18

Avg Thickness (in) 0.113 0.113 0.117 0.120 0.120 0.120 0.121 0.124 0.123 0.124 0.123 0.122 0.124 0.124 0.124 0.125 0.126 0.126 0.122 0.0039 3.2175 0.113 0.126 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00942 0.00942 0.00975 0.01000 0.01000 0.01000 0.01008 0.01033 0.01025 0.01033 0.01025 0.01017 0.01033 0.01033 0.01033 0.01042 0.01050 0.01050 0.0101 0.0003 3.2175 0.0094 0.0105 18

Strengthnorm [ksi] 4.909 5.129 5.036 5.806 5.146 5.689 4.572 4.695 4.687 4.655 4.836 4.511 4.585 4.856 4.705 4.743 4.700 4.995 4.90 0.3596 7.3342 4.51 5.81 18

73

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS1-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (QSBS)" 90° SPECIMENS FROM "UNT1" LAMINATES Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # A A A A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 1 1 MH1 1 1 MH1 1 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 4.66 4.69 4.69 4.77 4.61 4.73 4.17 4.11 4.31 4.14 4.08 4.12 3.97 4.03 4.05 3.96 4.00 4.08 4.29 0.3059 7.1347 3.96 4.77 18

Load (lbs) 185 182 184 193 187 193 167 170 177 172 171 172 162 168 167 169 169 173 176 9.394 5.3495 162 193 18

Avg Width (in) 0.254 0.252 0.252 0.252 0.252 0.253 0.249 0.250 0.250 0.252 0.252 0.252 0.253 0.251 0.249 0.252 0.250 0.251 0.251 0.0014 0.5494 0.249 0.254 18

Avg Thickness (in) 0.118 0.115 0.117 0.120 0.121 0.121 0.121 0.124 0.123 0.124 0.125 0.124 0.121 0.125 0.124 0.126 0.127 0.127 0.122 0.0034 2.7763 0.115 0.127 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.00983 0.00958 0.00975 0.01000 0.01008 0.01008 0.01008 0.01033 0.01025 0.01033 0.01042 0.01033 0.01008 0.01042 0.01033 0.01050 0.01058 0.01058 0.0102 0.0003 2.7763 0.0096 0.0106 18

Strengthnorm [ksi] 4.449 4.364 4.440 4.631 4.513 4.631 4.082 4.123 4.289 4.153 4.126 4.133 3.886 4.076 4.063 4.037 4.110 4.192 4.24 0.2163 5.1021 3.89 4.63 18

74

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS-MH-CTD MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (SBS)" 90° SPECIMENS FROM "FT" LAMINATES Tested Cold/Dry @ -65°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 14.04 14.36 13.87 13.71 13.73 13.49 13.63 13.47 13.06 13.56 13.51 13.46 12.70 12.29 12.55 12.69 12.06 12.22 13.24 0.6722 5.0752 12.06 14.36 18

Load (lbs) 588 608 582 576 578 567 561 553 537 562 557 554 514 518 509 531 507 514 551 30.275 5.4957 507 608 18

Avg Width (in) 0.252 0.251 0.250 0.250 0.250 0.250 0.250 0.249 0.251 0.249 0.249 0.251 0.250 0.250 0.250 0.249 0.250 0.250 0.250 0.0008 0.3209 0.249 0.252 18

Avg Thickness (in) 0.125 0.126 0.126 0.126 0.126 0.126 0.123 0.124 0.123 0.125 0.124 0.123 0.121 0.126 0.122 0.126 0.126 0.126 0.125 0.0016 1.3195 0.121 0.126 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01042 0.01050 0.01050 0.01050 0.01050 0.01050 0.01025 0.01033 0.01025 0.01042 0.01033 0.01025 0.01008 0.01050 0.01017 0.01050 0.01050 0.01050 0.0104 0.0001 1.3195 0.0101 0.0105 18

Strengthnorm [ksi] 14.199 14.639 14.139 13.976 13.997 13.752 13.564 13.514 12.997 13.714 13.554 13.395 12.433 12.529 12.388 12.936 12.294 12.457 13.36 0.7225 5.4077 12.29 14.64 18

75

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS-MH-RTD MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (SBS)" 90° SPECIMENS FROM "FT" LAMINATES Tested Dry @ 75°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 11.05 10.99 10.90 10.91 10.66 10.78 10.69 10.72 10.66 10.76 10.83 10.41 10.67 10.79 10.73 10.32 10.42 10.40 10.71 0.2069 1.9326 10.32 11.05 18

Load (lbs) 457 467 462 462 453 452 434 436 439 439 451 431 445 453 458 439 439 437 447 11.078 2.4759 431 467 18

Avg Width (in) 0.250 0.251 0.252 0.252 0.250 0.249 0.250 0.250 0.250 0.249 0.251 0.251 0.251 0.250 0.251 0.248 0.250 0.250 0.250 0.0010 0.4067 0.248 0.252 18

Avg Thickness (in) 0.124 0.127 0.126 0.126 0.128 0.126 0.122 0.122 0.123 0.123 0.124 0.124 0.125 0.126 0.128 0.128 0.126 0.126 0.125 0.0020 1.5629 0.122 0.128 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01033 0.01058 0.01050 0.01050 0.01067 0.01050 0.01017 0.01017 0.01025 0.01025 0.01033 0.01033 0.01042 0.01050 0.01067 0.01067 0.01050 0.01050 0.0104 0.0002 1.5629 0.0102 0.0107 18

Strengthnorm [ksi] 11.086 11.292 11.112 11.122 11.039 10.989 10.552 10.581 10.608 10.708 10.865 10.444 10.791 11.000 11.112 10.687 10.622 10.602 10.85 0.2530 2.3327 10.44 11.29 18

76

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS-MH-ETW MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (SBS)" 90° SPECIMENS FROM "FT" LAMINATES Tested Hot/Wet @ 200°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 6.17 6.47 6.34 6.28 6.15 6.28 5.14 5.35 5.23 5.47 5.53 5.33 5.47 5.56 5.44 5.21 5.16 5.02 5.64 0.4883 8.6506 5.02 6.47 18

Load (lbs) 260 269 267 267 261 267 211 217 211 227 229 220 230 235 228 221 222 211 236 22.117 9.3605 211 269 18

Avg Width (in) 0.251 0.248 0.251 0.251 0.250 0.250 0.250 0.250 0.249 0.251 0.250 0.251 0.251 0.250 0.251 0.249 0.251 0.249 0.250 0.0009 0.3692 0.248 0.251 18

Avg Thickness (in) 0.126 0.126 0.126 0.127 0.127 0.127 0.123 0.122 0.121 0.124 0.124 0.123 0.126 0.127 0.125 0.128 0.128 0.126 0.125 0.0021 1.6420 0.121 0.128 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01050 0.01050 0.01050 0.01058 0.01058 0.01058 0.01025 0.01017 0.01008 0.01033 0.01033 0.01025 0.01050 0.01058 0.01042 0.01067 0.01067 0.01050 0.0104 0.0002 1.6420 0.0101 0.0107 18

Strengthnorm [ksi] 6.290 6.596 6.463 6.453 6.319 6.453 5.115 5.281 5.120 5.488 5.548 5.304 5.576 5.713 5.502 5.395 5.344 5.117 5.73 0.5385 9.4036 5.12 6.60 18

77

MP1504 PWC1 MTM45-1-CF0525-36%RW

Testing completed as of 30 Jan 2006

AITR1392-8HQ-SBS-MH-ETW2 MTM45-1/4581-35% RW QUARTZ "INTERLAMINAR SHEAR (SBS)" 90° SPECIMENS FROM "FT" LAMINATES Tested Hot/Wet @ 250°F

ACG-UK TEST RESULTS normalizing tply [in] 0.0103

Specimen Number 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

ACG Batch # D D D A A A B B B B B B C C C C C C

ACG Cure Prepreg Cure Cycle Cycle Lot # Batch # MH1 4 1 MH1 4 1 MH1 4 1 MH2 1 2 MH2 1 2 MH2 1 2 MH1 2 1 MH1 2 1 MH1 2 1 MH2 2 2 MH2 2 2 MH2 2 2 MH1 3 1 MH1 3 1 MH1 3 1 MH2 3 2 MH2 3 2 MH2 3 2 Average Standard Dev. Coeff. of Var. [%] Min. Max. Number of Spec.

Strength [ksi] 5.41 5.37 5.26 5.08 5.21 4.95 4.57 4.68 4.24 4.39 4.59 4.50 4.72 4.83 4.81 4.44 4.57 4.53 4.79 0.3531 7.3784 4.24 5.41 18

Load (lbs) 228 223 209 215 220 209 189 195 174 183 188 187 198 203 203 185 195 193 200 15.038 7.5254 174 228 18

Avg Width (in) 0.251 0.252 0.252 0.249 0.250 0.252 0.250 0.251 0.250 0.250 0.250 0.250 0.250 0.249 0.251 0.248 0.250 0.250 0.250 0.0011 0.4291 0.248 0.252 18

Avg Thickness (in) 0.126 0.124 0.119 0.127 0.126 0.126 0.124 0.124 0.123 0.125 0.123 0.124 0.126 0.126 0.126 0.126 0.128 0.128 0.125 0.0021 1.7012 0.119 0.128 18

# Plies in Laminate 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 12 Averagenorm Standard Dev.norm Coeff. of Var. [%]norm Min. Max. Number of Spec.

Avg. tply [in] 0.01050 0.01033 0.00992 0.01058 0.01050 0.01050 0.01033 0.01033 0.01025 0.01042 0.01025 0.01033 0.01050 0.01050 0.01050 0.01050 0.01067 0.01067 0.0104 0.0002 1.7012 0.0099 0.0107 18

Strengthnorm [ksi] 5.515 5.387 5.064 5.220 5.311 5.046 4.585 4.695 4.219 4.440 4.568 4.515 4.812 4.924 4.903 4.526 4.733 4.691 4.84 0.3572 7.3783 4.22 5.52 18

end of mtm45-1 4581 quartz data -- nothing follows

78

WT-CTD

Warp Tension Properties (WT) -- (CTD) Strength & Modulus
MTM45/ 6K5HS AS4C Fabric Specimen Number CAJ1116B CAJ1117B CAJ1118B CAJ1226B CAJ1227B CAJ1228B CAJ2111B CAJ2112B CAJ2113B CAJ2114B CAJ2211B CAJ2214B CAJ2215B CAJ3115B CAJ3116B CAJ3117B CAJ3211B CAJ3212B CAJ3214B ACG Batch # A A A A A A B B B B B B B C C C C C C ACG Cure Cycle MH1 MH1 MH1 MH2 MH2 MH2 MH1 MH1 MH1 MH1 MH2 MH2 MH2 MH1 MH1 MH1 MH2 MH2 MH2 Prepreg Lot # 1 1 1 1 1 1 2 2 2 2 2 2 2 3 3 3 3 3 3 Cure Cycle Batch # 1 1 1 2 2 2 3 3 3 3 4 4 4 5 5 5 6 6 6 Strength [ksi] 127.924 124.281 124.199 124.220 118.859 130.362 127.187 125.727 125.469 118.746 131.372 129.312 126.032 121.641 126.135 134.082 127.169 129.769 125.359 Modulus [Msi] 9.005 8.985 9.301 8.887 8.981 9.217 9.193 9.606 9.317 9.383 9.618 9.441 9.131 9.042 8.932 9.244 9.185 8.976 Poisson's Ratio 0.055 0.051 0.065 0.063 0.066 0.067 0.060 0.064 0.071 0.066 0.062 0.058 0.057 Avg. Specimen Thickn. [in] 0.122 0.120 0.121 0.124 0.124 0.124 0.121 0.123 0.124 0.124 0.119 0.122 0.123 0.123 0.123 0.122 0.121 0.123 0.123 # Plies in Laminate 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 8 Failure Mode LWT/AGM/LWB LGT/LWB AWT/LGM LWB/LGM LWT/LWB/LGM LGM/LWB LWB/LWT LWB/LWB LGM/AGM LWB/LWT LWB LWB/LWT LGM LWB/LWT LWT/LWB LIT/LGM/LWB LWT/LWB DWB/AWB/LWT LIT/AGM/AWB Avg. tply [in] 0.01521 0.01505 0.01508 0.01545 0.01545 0.01548 0.01517 0.01535 0.01554 0.01549 0.01493 0.01530 0.01537 0.01534 0.01533 0.01527 0.01517 0.01534 0.01534

normalizing tply [in] 0.0153 Strengthnorm [ksi] 127.157 122.250 122.373 125.438 120.024 131.871 126.114 126.172 127.468 120.202 128.152 129.312 126.581 121.939 126.392 133.845 126.095 130.123 125.683 Modulusnorm [Msi] 8.951 8.838 9.164 8.974 9.069 9.324 9.115 9.640 9.465 9.498 9.382 9.482 9.153 9.060 8.916 9.166 9.210 8.999

0.054

Average 126.202 Standard Dev. 3.922 Coeff. of Var. [%] 3.107 Min. 118.746 Max. 134.082 Number of Spec. 19

9.191 0.222 2.416 8.887 9.618 18

0.061 0.006 9.235 0.051 0.071 14

Averagenorm 0.01530 Standard Dev.norm Coeff. of Var. [%]norm Min. 0.0149 Max. 0.0155 Number of Spec.

126.168 3.694 2.927 120.024 133.845 19

9.189 0.229 2.493 8.838 9.640 18

Prepared by NIAR COMPOSITES LABORATORY 2/29/2008

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