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Published byPeregrine Pitts Modified over 9 years ago
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NGST Mirror System Demonstrator from the University of Arizona Jim Burge B. Cuerden, S. DeRigne, B. Olbert, S. Bell, S. Clapp, P. Gohman, R. Kingston, G. Rivlis, P. Woida,
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UA technologies converge to NMSD
Large, fast primary mirrors NMSD technology for NGST 6.5-m f/ nm rms Adaptive secondary mirrors (thin glass, active control)
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Lightweight mirror using a thin reflective surface with active rigid support (high authority)
Rely on active control for shape accuracy. Use highly optimized lightweight backing structure for rigidity Choose facesheet for ease of manufacturing Use many position actuators, allows for redundancy
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The NGST Mirror System Demonstrator (NMSD)
2 meters in diameter 13 kg/m2 2 mm thick facesheet 166 actuators 35K operation Designed for launch 86 pounds total!
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Active mirrors Since the mirror shape is determined by active control, the emphasis shifts from the optical surface to the control system Wavefront sensing - This area is fairly mature. NASA, Lockheed Martin, and others have demonstrated accurate wavefront sensing directly from images using phase retrieval methods Actuators - The actuators are key. These devices can be made to be simple and robust. Also, The system design can accommodate failed actuators.
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NMSD Composite Support Structure Designed at UA and Lockheed Martin Fabricated at Composite Optics, Inc (COI).
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Cryogenic actuators Weighs < 50 g (including cabling)
80-pitch screw Electromagnetic drive Tunable step size from nm Excellent behavior at ambient and cryogenic
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The transition to actuator production
It took many months to develop a procedure and set of specifications that allow efficient actuator production We have completed and tested 180 units
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NMSD support structure - actuator installation
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Fabrication of glass membrane
The concept is to work the glass while it is rigidly bonded in place
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Glass substrate cast from Ohara E6 glass
Two pristine chunks of E6 Cast in UA 8-m spinning oven
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Completed casting from Ohara E6 borosilicate
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Fabrication of blocking body for NMSD membrane
Substrate 100 mm thick borosilicate casting Generate, grind, polish using conventional methods Ground to concave sphere, R = 20 m Supported with hydraulic actuators
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Fabrication of convex (back) side of NMSD membrane
Start with 40 mm thick blank Generate, grind, polish using conventional methods Polished to convex sphere, R = 20 m Supported with pitch pads on a convex blocking tool Carefully polished to assure removal of subsurface damage from generating and grinding
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Blocking of 2.2-m membrane
Membrane support Glass dam holding pitch Blocking body Hydraulic support Oven hearth
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Finishing 2 mm thick glass shell
Generate,grind and polish to thickness Completed 2 mm shell ~ 0.5 µm rms, but smooth
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NMSD Glass Deblocking Hot Oil-Bath Technique
Floats attached to glass Pitch softens and glass floats to the surface
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Preparations for deblocking
Set up “the hot shack” with 10’ insulated stock tank with heaters and circulation pump We went through a full scale test using float glass.
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The learning curve... Despite our positive test results, the silicone did not hold up at temperature, and the deblocking was aborted. We switched materials to solve this problem
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Successful deblocking
Floating in hot oil Lifting from the oil using 18-point whiffle tree attached to floats
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Cleaning and handling the glass
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The finished glass membrane
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Prepare for integration
Glass resting on support tool, convex side up Vacuum support tool
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A fracture of unknown origin
Crack tips found by etching then stop drilled Central site fully excised Site of fracture initiation The calculated Kt is 3.4, allowing ~900 psi stress. This would withstand launch and all handling operations as long.
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Actuator coupling to glass
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Bonding of attachment hardware
Pucks are attached with 12 µm thick bond of PRC 1564 Thickness maintained using microspheres Bond area controlled by controlling glue volume Puck positions maintained to 125 µm with template, tooling For safety factor of 3 for all loads in handling and operation: All pucks are proof tested at 1.45 lbs in shear Subloadspreaders are proof tested at 1.6 lbs in tension Additional coupons have been tested long term in vacuum at 3.5 lbs
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Attachment of primary loadspreaders
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Remaining tasks Complete loadspreader integration
Complete wiring and system testing electronics Coat optical surface Ambient testing at University of Arizona under tower Cryogenic testing at MSFC XRCF Operation using phase diversity wavefront sensing
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System Performance FE Analysis 27 nm rms
distortion due to cooling annealing residual strains blocking strains membrane support 27 nm rms Cryo distortions corrected by actuators, not by iterative polishing based on cryo measurements
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