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Successful Completion of the JWST OGSE2 Cryogenic Test at JSC Chamber-A While Managing Numerous ChallengesThe James Webb Space Telescope (JWST) Optical Telescope Element (OTE) assembly is the largest optically stable infrared-optimized telescope currently being manufactured and assembled, and scheduled for launch in 2018. The JWST OTE, including the primary mirrors, secondary mirror, and the Aft Optics Subsystems (AOS) are designed to be passively cooled and operate at near 45 degrees Kelvin. Due to the size of its large sunshield in relation to existing test facilities, JWST cannot be optically or thermally tested as a complete observatory-level system at flight temperatures. As a result, the telescope portion along with its instrument complement will be tested as a single unit very late in the program, and on the program schedule critical path. To mitigate schedule risks, a set of 'pathfinder' cryogenic tests will be performed to reduce program risks by demonstrating the optical testing capabilities of the facility, characterizing telescope thermal performance, and allowing project personnel to learn valuable testing lessons off-line. This paper describes the 'pathfinder' cryogenic test program, focusing on the recently completed second test in the series called the Optical Ground Support Equipment 2 (OGSE2) test. The JWST OGSE2 was successfully completed within the allocated project schedule while faced with numerous conflicting thermal requirements during cool-down to the final cryogenic operational temperatures, and during warm-up after the cryo-stable optical tests. The challenges include developing a pre-test cool-down and warm-up profiles without a reliable method to predict the thermal behaviors in a rarified helium environment, and managing the test article hardware safety driven by the project Limits and Constraints (L&C's). Furthermore, OGSE2 test included the time critical Aft Optics Subsystem (AOS), a part of the flight Optical Telescope Element that would need to be placed back in the overall telescope assembly integrations. The OGSE2 test requirements included the strict adherence of the project contamination controls due to the presence of the contamination sensitive flight optical elements. The test operations required close coordination of numerous personnel while they being exposed and trained for the 'final' combined OTE and instrument cryo-test in 2017. This paper will also encompass the OGSE2 thermal data look-back review.
Document ID
20160013558
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Park, Sang C.
(Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Brinckerhoff, Pamela
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Franck, Randy
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Schweickart, Rusty
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Thomson, Shaun
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Burt, Bill
(Genesis Engineering Solutions, Inc. Lanham, MD, United States)
Ousley, Wes
(Genesis Engineering Solutions, Inc. Lanham, MD, United States)
Date Acquired
November 17, 2016
Publication Date
July 10, 2016
Subject Category
Astronomy
Report/Patent Number
ICES-2016-330
GSFC-E-DAA-TN32058
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Vienna
Country: Austria
Start Date: July 10, 2016
End Date: July 14, 2016
Sponsors: International Conference On Environmental Systems, Inc., American Society of Mechanical Engineers, American Inst. of Chemical Engineers
Funding Number(s)
CONTRACT_GRANT: NAS5-02200
CONTRACT_GRANT: NNG14FC86T
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
JWST OGSE2 Cryogenic Test
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