DocumentCode
2913520
Title
A state diagram operations plan for James Webb Space Telescope cryogenic vacuum testing
Author
Diaz, Charles ; O´Rear, Patrick ; Reis, Carl
Author_Institution
Goddard Space Flight Center, JWST Obs., NASA, Greenbelt, MD, USA
fYear
2011
fDate
5-12 March 2011
Firstpage
1
Lastpage
30
Abstract
Space environment simulation testing can involve many complex and interdependent operations. A fundamental issue when defining these tests is the organization of information into a format that is understandable by reviewers and contributors. Plans are typically developed by simple combination of written procedures for individual systems. State diagram methodology was instead used to address the test definition problem for facility operations supporting a large-scale, long-duration space environment test of the James Webb Space Telescope (JWST) inside the Chamber A facility at NASA´s Johnson Space Center (JSC) in Houston, Texas. The state diagram technique selected for the JWST test is described and associated models are presented. This includes processes required to operate the cryogenic vacuum chamber and its support systems during both nominal and off-nominal conditions. Utilizing state diagram abstraction methods for JWST cryogenic vacuum test planning has facilitated refinement of the test processes and has expedited the orientation process for stakeholders with various technical backgrounds.
Keywords
aerospace instrumentation; aerospace simulation; aerospace testing; astronomical telescopes; cryogenics; vacuum measurement; Chamber A facility; James Webb Space Telescope cryogenic vacuum testing; NASA Johnson Space Center; cryogenic vacuum chamber; nominal conditions; off-nominal conditions; space environment simulation testing; state diagram abstraction methods; state diagram operations plan; test processes; Cryogenics; Hardware; NASA; Observatories; Telescopes; Testing; Vacuum systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2011 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-7350-2
Type
conf
DOI
10.1109/AERO.2011.5747660
Filename
5747660
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