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James Webb Space Telescope (JWST) Integrated Sciene Instrument Module (ISIM) Cryo-Vac 3 (CV3) Thermal Vacuum TestThis presentation describes the test objectives, test summary, test configuration and test performance of the James Webb Space Telescope Integrated Science Instrument Module CryoVac 3 Thermal Vacuum Test. Verify the ISIM System in its final configuration after environmental exposure and provide a post-environmental performance baseline, including critical ground calibrations needed for science data processing in flight.
Document ID
20160011456
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Packard, Ed
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 26, 2016
Publication Date
November 1, 2016
Subject Category
Ground Support Systems And Facilities (Space)
Fluid Mechanics And Thermodynamics
Report/Patent Number
GSFC-E-DAA-TN34924
Meeting Information
Meeting: AIAA WGSS Meeting
Location: Toulouse
Country: France
Start Date: September 20, 2016
Sponsors: Intespace
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Thermal Vacuum Testing
Space Simulation
Vacuum Performance
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