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The Infrared Astronomical Satellite (IRAS) hardware flight performanceAn overview of the cryogenic system design for IRAS (Infrared Astronomical Satellite) is presented along with the hardware flight performance. Specific flight performance parameters such as optics temperatures, initial stabilization times, and optics and cryogen system temperature profiles after depletion of the superfluid helium are highlighted.
Document ID
19860030627
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Urbach, A. R. (Ball Corp. Ball Aerospace Systems Div., Boulder, CO, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A15365
Funding Number(s)
CONTRACT_GRANT: NAS2-9700
Distribution Limits
Public
Copyright
Other

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