Definitions are given for spacecraft-surface thermal environment characteristics. Lumped-parameter thermal network modeling techniques are derived for spacecraft thermal environment analysis. The application of these techniques to thermal/vacuum testing is described. A major computer program required by these techniques is outlined. It is noted that this approach has been used to determine thermal environments for the Skylab ATM.
Spacecraft thermal environments.
01.01.1973
Sonstige
Keine Angabe
Englisch
Spacecraft thermal environments.
AIAA | 1973
|Spacecraft dynamic environments
NTRS | 1981
|