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Thermal Management of JWST Cryo-Vacuum Test Support EquipmentIn 2017, the James Webb Space Telescope (JWST) underwent functional testing and optical metrology verification of the combined Optical Telescope Element and Integrated Science Instrument Module (OTIS) under cryogenic vacuum conditions in Chamber A at the Johnson Space Center. The ground support and test equipment developed and tested over the previous decade to facilitate this test event were crucial elements of its success. Ground systems required for this test fall into several groups, including thermal simulators, mechanical support hardware, telemetry systems, and metrology systems. This paper will provide a summary of these systems, their development challenges, key features, and highlight thermal performance in the cryovac test.
Document ID
20180004566
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Havey, Keith A., Jr.
(Harris Corp. Rochester, NY, United States)
Cooke, Dwight A.
(Harris Corp. Rochester, NY, United States)
Huguet, Jesse A.
(Harris Corp. Rochester, NY, United States)
Day, Robert L.
(Harris Corp. Rochester, NY, United States)
Date Acquired
August 20, 2018
Publication Date
July 1, 2018
Subject Category
Instrumentation And Photography
Astronomy
Report/Patent Number
GSFC-E-DAA-TN58596
Meeting Information
Meeting: International Conference on Environmental Systems (ICES 2018)
Location: Albuquerque, NM
Country: United States
Start Date: July 8, 2018
End Date: July 12, 2018
Sponsors: UTC Aerospace Systems
Funding Number(s)
CONTRACT_GRANT: NNG11FD64C
CONTRACT_GRANT: NAS5-02200
CONTRACT_GRANT: JWST2012
Distribution Limits
Public
Copyright
Public Use Permitted.
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