The development and integration of 16 payload bay liner filters into the existing shuttle/payload contamination evaluation (SPACE) computer program is discussed as well as an initial mission profile model. As part of the mission profile model, a thermal conversion program, a temperature cycling routine, a flexible plot routine and a mission simulation of orbital flight test 3 are presented.
Orbiter/payload contamination control assessment support
1978-02-01
Report
Keine Angabe
Englisch
Orbiter/Payload Contamination Control Assessment Support
NTIS | 1978
|Support of the Boeing IUS in the Orbiter payload
AIAA | 1981
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British Library Conference Proceedings | 2000
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