SFPLIMP, Source Flow Plume Impingement Program, computes forces, moments, contamination, and heating rates caused by impingement of plumes on orbiting spacecraft from jets firing at high altitudes. User chooses among variety of configurations, data, and theories. Written in FORTRAN 77 and VAX DCL.
Computing Impingements Of Rocket Exhausts
NASA Tech Briefs ; 14 , 9
1990-09-01
Miscellaneous
No indication
English
Diffraction by Rocket Exhausts
NTIS | 1967
|Ionization in Afterburning Rocket Exhausts
NTIS | 1961
|Spacecraft contamination from rocket exhausts
AIAA | 1981
|Chemistry of lonization in Rocket Exhausts
AIAA | 1963
|Causes of ionization in rocket exhausts
AIAA | 1975
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