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Thermal Model Performance for the James Webb Space Telescope OTIS Cryo-Vacuum TestThe James Webb Space Telescope (JWST), set to launch in mid-2020, is currently undergoing a series of system-level environmental tests to verify its workmanship and end-to-end functionality. As part of this series, the Optical Telescope Element and Integrated Science Instrument Module (OTIS) Cryo-Vacuum (CV) test, the most complex cryogenic test executed to date by NASA, has recently been completed at the Johnson Space Center's Chamber A facility. The OTIS CV test was intended as a comprehensive test of the integrated instrument and telescope systems to fully understand its optical, structural, and thermal performance within its intended flight environment. Due to its complexity, extensive pre-test planning was required to ensure payload safety and compliance with all limits and constraints. A system-level pre-test thermal model was constructed which fully captured the behavior of the payload, ground support equipment, and surrounding test chamber. This thermal model simulated both the transient cooldown to and warmup from a 20 K flight-like environment, as well as predicted the payload performance at cryo-stable conditions. The current work is an assessment of thermal model pre-test prediction performance against actual payload response during the OTIS CV test. Overall, the thermal model performed exceedingly well at predicting schedule and payload response. Looking in depth, this work examines both the benefits and shortcomings of assumptions made pre-test to simplify model execution when compared against test data. It explores in detail the role of temperature-dependent emissivities during transition to cryogenic temperatures, as well as the impact that model geometry simplifications have on tracking of critical hardware limits and constraints. This work concludes with a list of recommendations to improve the accuracy of thermal modeling for future large cryogenic tests. The insight gained from the OTIS CV test thermal modeling will benefit planning and execution for upcoming cryogenic missions.
Document ID
20180004588
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
External Source(s)
Authors
Yang, Kan
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Glazer, Stuart D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Thomson, Shaun R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Feinberg, Lee D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Burt, William
(Genesis Engineering Solutions, Inc. Lanham, MD, United States)
Comber, Brian J.
(Genesis Engineering Solutions, Inc. Lanham, MD, United States)
Ousley, Wes
(Genesis Engineering Solutions, Inc. Lanham, MD, United States)
Franck, Randy
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Date Acquired
August 21, 2018
Publication Date
July 9, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC-E-DAA-TN58381
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Albuquerque, NM
Country: United States
Start Date: July 8, 2018
End Date: July 12, 2018
Sponsors: International Conference On Environmental Systems, Inc.
Funding Number(s)
CONTRACT_GRANT: NNG14FC86T
OTHER: 2018-545-JWST
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
Testing
OTIS
Modeling
OTE
ISIM
Thermal
Analysis
JWST
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