1 Spectrograph Mechanical Design

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					1 Spectrograph Mechanical Design

1.1 Overview
The NIFS spectrograph will be mounted in a duplicate of the NIRI cryostat and use a duplicate of the
NIRI OIWFS. The NIRI cryostat consists of a hexagonal vacuum jacket in which is supported a central
vertical cold work surface (CWS) which acts as an optical bench for both the science instrument and
the OIWFS (Figure 1). The NIFS spectrograph replaces the NIRI camera in the duplicate cryostat. A
pick-off mirror protrudes on a probe over the OIWFS to deflect the science beam into the spectrograph.
The discussion in this section concentrates on the mechanical design of the NIFS spectrograph. The
NIRI cryostat and OIWFS have been thoroughly analyzed by the NIRI design team. The recent
performance of NIRI is summarized in §Error! Reference source not found.6.6. Necessary
modifications to the duplicate NIRI components are discussed in §Error! Reference source not
found.6.




Figure 1: Detail of the duplicate NIRI cryostat with its vertical cold work surface near center, the
NIFS spectrograph mounted on the right, and the duplicate OIWFS mounted on the left

Detail of the NIFS spectrograph mounted in the duplicate NIRI cryostat is seen more easily in Figure 2.
In this view, the front and end sections of the hexagonal vacuum jacket have been moved aside to show
the spectrograph optical components and detector near the center of the figure. The hexagonal vacuum
jacket is ~ 1 m across. A large frame is mounted around the cryostat to carry two thermal electronics
enclosures and ballast for balancing the instrument. This frame is not shown in Figure 2, but is
discussed in §Error! Reference source not found.6.2.
            Figure 2: The NIFS spectrograph mounted in the duplicate NIRI cryostat.

All of the components shown in Figure 2 are extremely stiff in order to minimize deflection as the
entire two tonne instrument swings at the Cassegrain focus of the Gemini telescope. At the top of the
figure is the Instrument Support Structure (ISS) interface plate that attaches the instrument to the
Gemini telescope. The f/16.2 beam from the telescope enters the vacuum jacket via a window
protruding through the center of the interface plate. The hexagonal vacuum jacket is initially pumped to
a high vacuum and this vacuum is then maintained by cryopumping. Two large closed-cycle helium
coolers (not shown Figure 2) cool the internal components to ~ 60 K and cool the cryopump getters.
Cold and floating radiation shields (not shown in Figure 2) prevent radiation directly reaching the
spectrograph. The CWS plate is located directly behind the spectrograph in Figure 2. An 8 mm thick,
light tight, aluminum cover attaches to the CWS plate and encloses the spectrograph optics. On the far
side of the CWS plate is the OIWFS which acts as a closely-coupled near-infrared autoguider for the
spectrograph. The spectrograph proper begins on the far side of the CWS plate at the pick-off probe.
The input optics then pass the beam through a hole near the top of the CWS plate. The small science
field then passes to the IFU which slices the field into strips and stacks the strips end-to-end to form a
long staircase slit. This long slit is fed to a medium resolution spectrograph that delivers spectra to the
detector at the lower right of the CWS plate.

1.2 Cold Work Surface Plate
All of the NIFS optical components are carried on the 40 mm thick cold work surface plate. This plate
is a modified version of the NIRI CWS plate, heavily modified on the science instrument side to carry
the NIFS spectrograph but largely unchanged on the OIWFS side. Three V-shaped titanium tines
support the CWS plate at the center of the vacuum jacket. These tines are very stiff and limit relative
movement between the plate and the telescope. The titanium tines restrict heat inflow to the instrument
and flex inwards by more than 3 mm as the CWS plate shrinks in cooling to 60 K.

Most of the NIFS spectrograph components are carried in a plane 90 mm above the CWS plate. They
are cantilevered off the plate in optical table style. Figure 3 shows a view of the NIFS spectrograph
looking onto the CWS from the science side of the plate. The figure is labeled with the main
components of the spectrograph. The Focal Plane Mask Wheel is on the far side of the CWS plate and
the optical beam passes inwards through the CWS plate to the spectrograph on this side. The beam then
zigzags down through the IFU and spectrograph components to the detector. The extensive black sheet
metal baffling that will be required between the folded optical system is not shown in Figure 3. This is
needed to absorb scattered light. Where possible flat sheet sections with cut outs that graze the beam
will be used to approximate an infinite cavity baffle. Particular care will be taken to baffle the grating
and image slicer as these are expected to be the largest sources of scatter in the instrument. A sheet
metal “zero order” trap is included to suppress direct reflection from the high dispersion gratings.
           Figure 3: NIFS spectrograph optics mounted on the cold work surface plate.


1.2.1 Stability (Flexure)
NIFS is far lighter than NIRI and will place far smaller forces on the CWS plate and titanium support
tines. The 8 mm thick aluminum cover over the NIFS spectrograph will add significantly to the
stiffness of the plate. Once all the optical mounts are in place on the CWS plate and aligned, a 3 mm
thick plate may be attached across the top of all of them. This would tie the entire opto-mechanical
system together to form a very stiff structure. RSAA will continue flexure analysis during the course of
the instrument design.

1.2.2 Thermal Conductivity Issues
Although the NIFS instrument is far lighter than NIRI and will cool faster, it is likely that the
temperature difference across the CWS plate will remain as for NIRI. This is largely due to the
unchanged heat load on the edge of the plate coming from the radiation shields. The current cold test of
NIRI (Feb 2000) suggests that this temperature difference is ~ 5 K from center to edge of the plate.
This should not cause major problems for NIFS. RSAA will continue thermal analysis during the
course of the instrument design.

1.3 Spectrograph Pick-Off Probe
Figure 4 shows a cross section through the CWS plate in the vicinity of the input beam. The
cantilevered pick-off probe shown in the figure protrudes through a cylindrical baffle above the
OIWFS and folds out the NIFS science field. This small part of the telescope field comes to focus at
the Focal Plane Mask Wheel. The cylindrical baffle around the probe passes the full 3 telescope field
to the OIWFS and prevents scattered light from entering the cavity surrounding the OIWFS. NIFS does
not use the NIRI beamsplitter wheel so without the baffle there would be large scatter into this cavity.
The baffle is carried by the OIWFS radiation shield and it does not contact the pick-off probe. The
pick-off probe is cantilevered closely from the CWS plate in order that it be as stable as possible with
respect to the spectrograph and to ensure that it becomes as cold as possible.
                       Figure 4: NIFS OIWFS baffle and pick-off probe area.


1.3.1 Field-of-View and Baffling
The NIFS field is ~ 2 mm square and the pick-off probe is ~ 94 mm above the telescope focus. Rays
passing by the probe continue to the OIWFS. The probe is 10 mm thick and carries two small diamond
turned aluminum mirrors at the center of the telescope field, the upper of these mirrors folds out the
NIFS science field. The closest usable unvignetted guide star to the center of the NIFS field is at a little
over 8 mm or 12.7 from the field center (Figure 5). Guide stars will pass through to the OIWFS at a
little over 5 mm from the field center, but will be partially vignetted and will not properly illuminate
the two-part focus prism in the OIWFS. The OIWFS will not then deliver accurate focus corrections to
the telescope. There may be usable position angles where the prisms are equally illuminated but this
would require that the object be rotated with respect to the NIFS slit and this may not be scientifically
desirable.
              Figure 5: NIFS pick-off probe showing OIWFS guide star availability.

The cantilevered pick-off probe is drilled with a stepped hole to tightly baffle the NIFS science field
through to the Focal Plane Mask Wheel. Bright stars near the science field will scatter light into the
drilled hole inside the pick-off probe. Scatter inside the pick-off probe is of considerable concern.
Preliminary analysis with the OptiCAD non-sequential ray tracing package is shown in Figure 6. This
figure shows rays reflecting off the probe mirror and both passing through the probe to the top and
scattering off the OIWFS baffle. The models used in this analysis are in stereo-lithographic format (.stl)
composed of interlocking triangles. Tracing such a complex object with these files has proven to be
difficult. We will soon be able to transfer IGES solid body objects to OptiCAD and will continue
scattered light analysis of this area of NIFS.




             Figure 6: OptiCAD scattering analysis of the NIFS pick-off probe region.


1.3.2 Wavefront Sensor Test Projector
A second diamond turned mirror, facing downward from the end of the probe, folds a beam from a test
projector built inside the probe to the OIWFS. This projector creates a star image at the focal plane of
the telescope directly under the probe that will allow the OIWFS to be tested during daytime or when
NIFS is not on the telescope. This feature is discussed in more detail in §Error! Reference source not
found.6.5.2.1.

1.3.3 Stability (Flexure)
It is essential that deflection of the pick-off probe not cause significant star movement in the NIFS
focal plane. Deflection of the probe shown in Figure 5 has been analysed. Although tapered, during
analysis the probe was assumed to be parallel and of the smallest cross section (5410 mm). Analysis
using standard case formulae for the 175 g probe showed a deflection of ~ 1m at the probe tip. While
parallel deflection of the pick-off probe will not cause focal plane shift, rotation of the mirror will.
Analysis showed a rotation of 6.3 rad that would result in an image shift of about 1 m in the
telescope focal plane or ~ 1 mas. The probe is very stiff in the shear direction; the calculated shear
deflections are just a few nanometers in any direction. Table 1 shows the working formulae for these
results.

                         Table 1: NIFS Pick-Off Probe Deflection Summary
  Probe Material 6061 Aluminium Alloy:

                                    Volume                64680       mm3
                                      Mass              174.636         g            SG (6061 Al) = 2.7
                                   Force, W           0.1749.8         N
                                  Breadth, b                 54       mm
                                   Depth, d                  10       mm
                                   Length, l                 84       mm

          Section properties across 10 mm.                 4500       mm4
                             Ixx = (bd3)/12

     Deflection in bending under self load.       -4.06876E-04         mm E (6061 Al) = 69 000 MPa
                       y = (Wl3)/(8EIxx)

          Slope in bending under self load.        6.30987E-06     radians            Reference: Roark
                        = (Wl2)/(6EIxx)

                     Position shift at focus.      6.37928E-04         mm                    L = 101.01
                                     z = L

                           Shear deflection.       4.84658E-06         mm          Reference: Shanley
                          = (wl2)/(2AG)                                   G (6061 Al) = 26691 MPa
                                                                               w = W/l = 0.0198 N/mm
                                                                                          A = 540 mm2




1.4 Spectrograph Focal Plane Mask Wheel
A twelve position Focal Plane Mask Wheel is located at the folded telescope focus. The wheel is
completely enclosed in a cold aluminum housing carried on the OIWFS side of the CWS plate and
directly attached to it. The wheel rotates on lubricant-free stainless steel ball bearings and is driven and
locked using a miniaturized version of the NIRI drive system. Magnetic encoding of the type used in
NIRI will encode the wheel (§Error! Reference source not found.7.1). Drive and position locking of
this small wheel are critical especially when occulting disk inserts are in use. The locking mechanism
will be the subject of substantial design evaluation.

1.4.1 Mask Inserts
The focal plane wheel carries a clear aperture for general integral-field spectroscopy plus an array of
masks for special uses and a blank to form an instrument shutter. Apart from the clear mask which will
be an open frame, all other masks will be metalized sapphire or glass disks. Each disk will be 6 mm in
diameter and 0.5 mm thick. Mask patterns will include occulting disks of various sizes, holes to
simulate stars, and a Ronchi screen for calibrating the spectrograph. The wheel will initially be placed
under an alignment microscope in order to align the occulting disks and Ronchi screen. This should be
a once only operation.

1.5 Spectrograph Input Optics
The NIFS input optics include the focal ratio converter mirror, the cold stop mirror, and two fold
mirrors. These two fold mirrors fold the long f/256 beam to the image slicer. If tests show suitably low
scattering values can be achieved then all four mirrors will be machined in 6061 aluminum alloy with
integral mount and adjustment points and have diamond turned and coated optical surfaces. As most
NIFS parts are 6061 alloy, the mirrors and mounts should shrink by the same amount with cooling and
should retain alignment.

The 4 mm diameter cold stop mirror will be directly mounted to a cold housing without adjustment.
This small mirror is diamond turned without edge chamfer to provide a sharp edge to cleanly cut off
the telescope pupil. A black painted 1 mm wide cavity is formed in the housing around the cold stop to
provide a beam dump for rays outside the telescope pupil. Both the focal ratio converter mirror and the
cold stop mirror are deeply buried in an aluminum housing. Small stepped holes provide tight baffling.
This baffling prevents rays from passing under the focal ratio converter mirror, by-passing the cold
stop, and reaching the image slicer directly.

1.5.1 System Adjustment
Two of the four input mirrors will be adjustable (Figure 7). The focal ratio converter mirror has a three
point mount adjustment to steer and focus the re-imaged telescope pupil onto the fixed pupil mirror.
One of the two fold mirrors has a three point mount to steer the re-imaged f/256 focus onto the center
of the image slicer.
Figure 7: NIFS input optics showing the Focal Plane Mask Wheel, focal ratio converter mirror,
cold stop mirror, and Filter Wheel.


1.6 Spectrograph Order Sorting Filter Wheel
An eight position filter wheel carries the spectrograph order sorting filters and is supported in a housing
mounted on the science side of the CWS plate. This housing tightly baffles the wheel and prevents out-
of-band light from entering the spectrograph space. The filters are carried as near as possible to the
cold stop to maximize the beam footprint through the filters and prevent point defects in the filters from
skewing the bandpass to any one point in the spectrograph field. This housing also carries both of the
input fold mirrors. The filter wheel drive and encoding system will be similar to that used in NIRI with
Phytron stepper motor drive and magnetic encoding (§Error! Reference source not found.7.1). Filters
are accessible from, and may be changed by, removing the vacuum jacket end plate, floating shield,
radiation shield, and spectrograph cover. An extensive strip down of the vacuum jacket is not required.

1.7 Spectrograph Integral-Field Unit

The IFU reformats the 3.03.0 NIFS field into 29 separate 0.1 wide slitlets and joins the slitlets end-
to-end to form a long staircase slit for input to the NIFS spectrograph. The IFU parts are carried above
the CWS plate on separate brackets; IFU-1 carries the image slicer, and IFU-2 carries the pupil and
field mirror arrays. At assembly, the tops of these brackets are tied together with a cross-plate to stiffen
the IFU structure.

1.7.1 Image Slicer
The NIFS IFU image slicer is constructed from a stack of 1.0 mm thick aluminum sheets clamped
together in a frame. This stack is then diamond machined across the edge of the stack to form a flat
surface and then diamond machined to a shallow concave sphere in the center of the stack. The stack is
then released, each slice is rotated by a small angle then the stack is re-clamped. We envisage using a
pinned or machined staircase system for controlling the slice rotation. Figure 8 shows the image slicer
mirror stack after diamond machining of the spherical mirror shape and after the mirror stack has been
rotated. The slicer assembly is carried from the CWS plate on the IFU-1 support. The slicer assembly is
adjustable in rotation about two axes to steer the 29 separate telescope pupils onto the 29 mirrors of the
pupil mirror array.
Figure 8: IFU image slicer stack after machining of the spherical optical surface. The stack is
shown aligned for machining (top) and after each slice has been rotated (bottom).

A half-size pinned prototype image slicer has been constructed to demonstrate the feasibility of this
approach. The alignment of the prototype was tested on an optical bench and shown to be acceptable.
However, it will be necessary to construct a prototype to the specification of the concentric IFU design
to convincingly establish the viability of this approach.

A machined staircase is an alternative assembly system. This can align all the slicer mirrors from one
master surface to the required 30 rad angular tolerance slice-to-slice. Figure 9 shows part of the
staircase assembly system. The surrounding housing has been omitted for clarity. The part shown here
forms the front of the slicer housing and is machined in one piece from 6061 aluminum alloy to match
the expansion of the mirrors. The master surface and the two opposing staircases are machined in one
operation to maintain accuracy. Opposite pairs of defining edges on the staircases are 54 mm apart and
the step-to-step height is ~ 57 m and varies a little from the central slice towards the top and bottom
slices. To meet the 30 rad tolerance, the required step accuracy is ~ 1.6 m per span or 0.8 m per
step. This should be feasible on a good quality CAM milling machine.

At assembly, each of the 29 slices in the stack is placed gently down onto two defining edges, one on
each staircase. Each slice rotates around the common focal line that passes down the center of the
stack. The mirrors face the staircase and each mirror touches the staircase defining edges on the flat
diamond turned areas adjacent to the mirror, and spans the beam aperture. This beam aperture defines
the length of each slitlet and hence the field of the IFU. It must be accurately machined. Stops in the
surrounding housing align the slices endways to the necessary 30 m. Anvils on the top and bottom of
the stack and rods through the holes in the stack are then clamped to form a permanent assembly.
                        Figure 9: Staircase image slicer alignment system.


1.7.2 Pupil Mirror Array
Both the pupil and field mirror arrays are diamond turned into similar 6061 aluminum alloy blanks.
Figure 10 shows detail of these blanks. The blanks are roughed to shape on a CAM milling machine,
then transferred to a CAM diamond turning machine with x,y,z axis control. A spinning fly-cutter then
generates 29 slightly toroidal, concave pupil mirrors. Figure 11 shows the mirror cutting procedure.
The spinning fly-cutter is represented by the flat disk. The curved edge of the disk represents the
industry standard diamond tip radius of 0.76 mm which produces a smooth finish. The center of the
spinning cutter follows the looping CAM path shown in Figure 11 and cuts the 29 mirrors on a 448 mm
radius. There are no steps between the mirrors.
Figure 10: Detail of pupil and field mirror array blanks.
Figure 11: NIFS pupil mirror generation procedure. The top figures show the pupil mirror blank
and the path of the fly-cutter. The lower-left figure shows the blank rotated by 4°. The lower-
right figure shows the looping CAM path. The vertical paths follow the curve of the mirror.

This fly-cutting procedure does not generate a true spherical surface (§Error! Reference source not
found.4.21). To minimize departures from a sphere, the array blank is rotated in a jig by 4° to place the
two equators of the generated spheres at the center of the mirrors. This generation process requires that
all three axes of the diamond turning machine to be active for all but the center mirror. This process
requires a freeform generator such as the Moore 500FG DT machine and there are relatively few of
these in the world.

A simplified version of the required tool path has been programmed and executed on a prototype pupil
mirror array using a CAM milling machine at RSAA with acceptable results. A much more elaborate
tool path would be required to manufacture the actual pupil mirror array.

1.7.3 Field Mirror Array
The field mirror array is generated in a similar manner to the pupil mirror array. All the mirrors are
spherical with a radius of 60.834 mm. This array is convex about the image slicer and compliments the
concave pupil mirror array. Figure 12 shows the crowded region around the pupil and field mirror
arrays mounted on the IFU-2 support structure.
Figure 12: NIFS IFU-2 assembly carrying the pupil and field mirror arrays. The triple fold
mirror is seen at right.

A prototype linear field mirror array was produced with a CAM milling machine at RSAA. While
demonstrating the feasibility of the approach, a much more elaborate tool path is needed to
manufacture the actual field mirror array.

1.7.4 Triple Fold Mirror
The three principal arms of the NIFS optical system are longer than the CWS plate is wide. The triple
fold mirror (Figure 13) folds all three arms of the optical system into the vacuum jacket from one
multi-faceted mirror. This mirror is constructed from a 90 mm square piece of 6061 aluminum alloy
with mounting points directly machined into the blank. All three flat mirrors are diamond turned into
the blank in one accurate operation in a diamond turning machine of the type used to cut polygon scan
mirrors. The triple fold mirror is mounted to the IFU-2 support structure without adjustment.




                           Figure 13: NIFS triple fold mirror schematic.


1.8 Spectrograph Collimator
NIFS uses a de-centered Bouwers optical system as a spectrograph collimator. The collimator consists
of a spherical primary mirror and a concentric meniscus corrector lens. The meniscus is manufactured
from a calcium fluoride disk ~ 100 mm in diameter, two opposite sides of the blank are then trimmed
to leave the 55 mm wide meniscus. The meniscus is mounted with respect to the de-centered camera
axis and appears tilted in the optical layout. A compliant mount that allows for temperature induced
strain carries the meniscus and allows for some coarse x,y adjustment on the cold work surface. The
lens has little power so we do not envisage that any z adjustment will be required.

With a reflective surface measuring 16070 mm, the collimator primary mirror is the largest optical
component in NIFS. We envisage diamond turning the mirror from 6061 aluminum alloy for two
reasons; Firstly, no mirror cell is required and the three point mount is machined directly into the
aluminum blank before diamond turning. This provides a more stable mount for this large component
than a glass mirror in a cell. The three point adjustment system is necessary to both focus and properly
center the grating pupil on the grating. Secondly the aluminum mirror will shrink in step with the
aluminum cold work surface. This will allow us to focus the collimator onto the pupil mirror array
using an optical table at ambient temperature and have it retain focus at 60 K. The mirror has a focal
length of 434.3 mm and the temperature induced change of focal length is 1.76 mm at 60 K. A
temperature difference of 5 K between the aluminum mirror and the cold work surface will defocus the
collimator by 13 m. This should have little effect on total image quality

1.9 Spectrograph Grating Wheel
NIFS carries seven gratings and one mirror in a large grating wheel. This is the largest and heaviest of
the three wheels in the spectrograph. The wheel uses a replica of the NIRI wheel drive and locking
system, the gear is driven from a Phytron stepper motor, and a NIRI-style magnetic encoding system is
used.

All seven gratings and the one mirror are replicated on 6061 aluminum alloy blanks (Figure 14). A
three point adjustment is machined directly into each blank to allow each grating in turn to correctly
place spectra onto the detector. Most of the gratings fill the detector completely so the adjustment
points are as far apart on the blanks as is possible in order to make for a sensitive adjustment system.
The reflective surface of the mirror is parallel to the back of the blank. Each grating blank in turn is
machined with the required grating angle with respect to the back of the blank. Each blank is
individually fitted with a sheet metal mask to limit the diffracted pupil size as seen from the collimator.
Figure 15 shows the complete grating wheel. The gratings are skewed on the wheel face in order to
place the wheel as near to the CWS plate as possible for stability reasons.




                             Figure 14: NIFS grating and mirror blanks.
                            Figure 15: NIFS spectrograph grating wheel.

Each of the gratings and mirror has a mass of about 300 g giving a total mass of 2.4 kg. These eight
gratings plus the 2.5 kg wheel rotate on preloaded deep groove ball bearings that are lubricated with
vacuum spluttered moly-disulphide lubricant. These bearings are ~ 80 mm in diameter, have a ~ 80 mm
track spacing, and are preloaded in X configuration to about three times the 48 N force applied by the
mass of the components. A total pre-load of 145 N is small for bearings of 80 mm diameter even when
dry lubricated.

The NIFS spectrograph camera has a focal length of 288 mm and a detector with 18 m pixels. To
meet the Gemini requirement that the image be stable to 0.1 pixel per 15° change in attitude, angular
grating movement must not exceed 3 rad with respect to the camera. This is a demanding but
acheivable condition. It requires that the bearing and latching system be preloaded to eliminate
backlash, and that the wheel and mounting structure be very stiff to avoid excessive gravitational sag.
The gratings also need to be stable to at least this tolerance on their three point adjustable mounts.
Indeed, similar levels of stiffness are required in many areas of the instrument.

We may be able to apply extra bracing to the edge of the wheel in at least one direction, most likely the
spectral direction with a modification to the NIRI style wheel mechanism. The NIRI mechanism uses a
narrow lock arm rotating on a flexure pivot. We may be able to make the NIFS grating lock arm
triangular with flex pivots in two corners of the triangle. With strong spring pressure on the lock arm
we can stabilize the edge of the wheel in one direction to the required tolerances of about 3 rad.
RSAA will continue to investigate this area as the NIFS design progresses.

1.10 Spectrograph Camera
All five elements of the refractive spectrograph camera are elastically mounted in a single aluminum
tube. This tube is carried in turn by brackets from the CWS plate. A tongue and groove system allows
the camera to be easily removed and replaced on the cold work surface and maintains alignment to the
detector. This alignment groove in the cold work surface extends under the detector package to
maintain alignment between the camera and detector housings. The input end of the camera abuts the
sheet metal zero order trap and the output end carries part of a labyrinth seal to seal the camera to the
detector housing but does not touch the detector housing. The interface between the end of the lens
housing tube and the camera will receive considerable design attention as it is important that it not leak
radiation directly to the detector.

1.11 Spectrograph Detector Package
Figure 16 shows plan and elevation views of the proposed detector mounting arrangement. At
assembly, the ceramic package for the Rockwell HAWAII-2 detector is inserted in a 1919 Pin Grid
Array socket carried on the multi-layer detector circuit card. This card is then placed in the detector
housing, the ceramic package is pressed against a Macor ceramic defining-ring, and the card is spring
loaded to maintain contact between the package and the ring with cooling. The detector housing is a
6061 aluminum alloy box with removable top and side panels. A protruding tongue on the bottom of
the box mates with the alignment slot in the CWS plate to maintain camera to detector alignment. The
defining ring has no tip-tilt adjustment with respect to the detector housing but is pre-aligned on an
optical table using an empty ceramic package. The detector housing is positioned when warm and then
repeatedly cold tested for proper focus. Two strip clamps along the top and bottom edges of the
housing clamp the detector housing to the CWS plate. Push-pull screws and a small micrometer fitted
to the CWS plate will aid the focus setting.




                     Figure 16: NIFS science detector mounting arrangement.

The Rockwell HAWAII-2 detector is cooled by conduction through the central 15x15 pins of the Pin
Grid Array socket. Heat passes along solid copper wires soldered to each of the central pins, these
wires loop to adjacent copper blocks. Heat now passes from the blocks to copper braids, through a
labyrinth light seal in the lower housing wall, to the second stage closed-cycle helium cooler
connection located 80 mm from the detector housing.

Figure 17 is a plan view of the detector housing, braid, and ribbon cable systems. Low capacitance
electrical ribbon cables begin at plugs on the lower corner of the circuit card and pass to a hermetic
connector on the nearest point of the vacuum jacket center section. These ribbon cables consist of very
narrow copper tracks printed on and between black woven Teflon fabric. The ribbon cables pass down
from the circuit card, through a labyrinth seal in the rear wall of the detector housing, through a second
labyrinth on the NIFS cover, through a third labyrinth under the radiation shield, through a slot in the
floating shield, then to the hermetic connector. Each of these labyrinth seals provides successive light
sealing and thermally shunts heat inflowing along the ribbon cables to the CWS plate. The SDSU
detector controller is mounted vertically on the vacuum jacket center section. It is necessary to place it
near the science side closed-cycle helium cooler. Fortunately the cooler microstepper drive motor, with
possible stray magnetic fields and RF interference, is on the far side of the cooler and should not affect
the SDSU controller. Special precautions will be taken to shield the input wiring to the controller.
                           Figure 17: NIFS detector to controller cabling.


1.12 Spectrograph Cover and Vent
A cast and fully machined 6061 alloy cover 8 mm thick will cover the NIFS spectrograph and make a
light-tight seal to the CWS plate. Two cable labyrinth fittings located in the edge of the cover will
allow cable access for the detector and the two mechanisms inside the cover. Lifting points on the
cover will make for easy handling during instrument assembly.

During vacuum pumping or unintended air admission, the NIFS cavity will not be able to breathe with
sufficient flow rate through the pick-off-probe and past the focal plane wheel. This could apply
destructive forces to the spectrograph cover. A high capacity baffled vent on the cover will allow direct
air admission through the cover and prevent any damage to the spectrograph.

1.13 Spectrograph Mechanical Design Risks

1.13.1 Spectrograph Flexure
The spectrograph optics must be held accurately to meet the Gemini requirement of < 0.1 pixel flexure
per 15° change in attitude. The large grating wheel has been identified as a particular concern.
However, similar levels of stiffness are required in many areas of the instrument. This should be
achievable with careful design followed by empirical adjustment.

1.13.2 Spectrograph Alignment
The telescope pupil must be accurately aligned to the 4 mm diameter cold stop to reduce thermal
emission from the telescope in the K band. There is no active adjustment of the cryostat orientation at
the telescope. This adjustment will have to be made by mounting an alignment telescope on the ISS
interface plate and visually setting the adjustment of the focal ratio converter mirror when the
instrument is warm. The adjustment will be checked when the cryostat is cold by sighting the cold
stop.
Alignment of the IFU image slicer elements and of the pupil and field mirror arrays will be particularly
crucial. Two alternative mounting arrangements for the image slicer elements have been proposed; a
pinned system, and a machined ramp system. These will be tested further. Alignment risks for the
mirror arrays will be mitigated by manufacturing the arrays as monoliths.

Procedures for aligning the cold stop, IFU, and spectrograph optics will be developed using a setup
copy of the CWS plate at room temperature. The aligned optical components will later be transferred
to the cryostat and re-aligned.

1.13.3 Spectrograph Baffling
Elimination of stray light is crucial for achieving ultimate performance at J and H. Light entering the
science instrument must be efficiently baffled at the cold stop, and light scattered within the
spectrograph must be eliminated by light baffles. The scattering properties of proposed designs will be
modeled using the OptiCAD non-sequential ray trace program.