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
110 pages
Report
Keine Angabe
Englisch
Payload/orbiter contamination control assessment support
NTRS | 1975
|Orbiter/payload contamination control assessment support
NTRS | 1978
|Payload/Orbiter Contamination Control Assessment Support
NTIS | 1975
|Orbiter/payload contamination control assessment support
NTRS | 1977
|Orbiter/Payload Contamination Control Assessment Support
NTIS | 1977
|