Two computer programs calculate interaction effects of high speed spacecraft on the environment at altitudes from 90 km to 150 km. EXT program determines fluid field in bodies of arbitrary geometries in transient flow regime. INT program uses EXT output and measures flow conditions inside spacecraft body.
A low-altitude satellite interaction study
1971-12-01
Miscellaneous
No indication
English
NTIS | 1968
|Satellite altitude determination uncertainties
NTRS | 1971
|Satellite altitude control systems
Engineering Index Backfile | 1963
|