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Space Shuttle's orbital environmentVariations with the solar cycle of chemical composition, density and temperature of the orbital environment of the Space Shuttle are reviewed; micrometeoroid fluxes, ionizing radiation, photon fluxes and cosmic ray bombardment to which the Shuttle will be subjected are also mentioned. In addition, gases arising from offgassing and outgassing of contaminants (at about 300 K) from the Shuttle are considered, and particulates ejected during rocket firings or from the leakage of pressurized vessels (i.e., the cabin) are taken into account.
Document ID
19780035556
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Witteborn, F. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Simpson, J. P.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
December 1, 1977
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
78A19465
Distribution Limits
Public
Copyright
Other

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