AMTD-II test preparation · 2019-01-30 · AMTD-II test preparation 11-18-2014 Ron Eng, Marcus...
Transcript of AMTD-II test preparation · 2019-01-30 · AMTD-II test preparation 11-18-2014 Ron Eng, Marcus...
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AMTD-II test preparation
11-18-2014
Ron Eng, Marcus Baker, Harlan Haight, William Hogue, Jeff Kegley, Richard Siler, John Tucker, Ernest Wright
NASA Marshall Space Flight Center
Mirror tech days
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Objectives
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Perform optical test from 293º to 253º
Kelvin (~20º to -20º C) to validate thermal
model.
Perform vibration and acoustic test to
validate model.
Facility modification is underway.
Goal: readiness in 2015.
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AMTD-II mirrors
ROC (m) dia. (m) R/#
Schott Zerodur 3.2 1.2 R/2.67
Exelis ULE 3.5 1.5 R/2.3
Xinetics SiC 16 1.35 R/11.8
Current large > 3.5 < 4.25 slower than R/2.7
chamber test
configuration
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> 3.5m ROC and slower than R/2.7
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X-ray cryogenic facility (XRCF)
History
Testing grazing-incidence x-ray telescopes (Chandra,
Solar X-ray Imager, Solar B) since 1992.
Cryogenic optical interferometric testing of normal
incidence, visible & IR telescope optics & components
since 1999.
Large test chamber:
7.3 x 22.9 m (O.D. x L) horizontal
cylinder
6 x 18.3 m (I.D. x L) test volume
4.25 x 9.4 m (I.D x L) Helium shroud
527 m: x-ray guide tube
Cryo shroud enclosure: 20K to 320K
Refrigeration system: 2 gaseous
helium refrigerators; each capable of
~1 kW at 20K.
Vacuum systems: 10-8 Torr
Clean Rooms:
6000 sq. ft. Class 2,000
2000 sq. ft. Class 10,000
Onsite machine shop
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JWST PMSA test configuration
4 m dia., 16 m ROC
6 x 18.3 m test volume
4.25 m dia. Helium cooled shroud
2 closed-loop helium cryo systems
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JWST mirror segments at XRCF
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XRCF clean room
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1x3 m optical test chamber
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Vacuum Chamber: 1x3 m cylinder with helium shroud.
Optical View Ports: BK7 window; 150 mm dia. clear aperture.
Precision stage to provide interferometer pointing and alignment.
Operational Pressure: < 5 E-6 Torr
Temperature Range: 300 to 12K
Typical cryo optical test: 290, 200, 100, 70, 50, 30K, 2 cycles; 3
weeks duration.
CryoOptical Test Chamber
Shroud Verification Test
0
25
50
75
100
125
150
175
200
225
250
275
300
0 1 2 3 4 5 6 7 8 9 10
Elapsed Time (hrs)
Te
mp
era
ture
(K
elv
in)
Cylinder Average
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Pressure tight enclosure (PTE) = R/1
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Proposed AMTD-II mirror test configuration
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Pressure tight enclosure (PTE) test configuration
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PTE optical windows
150mm clear aperture
BK7 window
100mm sapphire window
• IR camera
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Test plans
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• Repeat stack core mirror optical test in small chamber
with front to rear thermal gradient.
• Modal test with interferometer.
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Thermal IR image
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Improve IR thermal capability to record temperature gradient.
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JWST Backplane stability test article (BSTA)
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PhaseCam 5010 interferometer with
modal capability
• 1954 x 1967 pixels
• Effective array: 977 x 983 pixels
• PV uncalibrated accuracy: 15 nm
• RMS uncalibrated accuracy: 3 nm
• PV repeatability:0.24 nm
• RMS repeatability: 0.05 nm
• PV precision: 2.64 nm
• RMS precision: 0.51 nm
Optical test instrument
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