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
Sonstige
Keine Angabe
Englisch
Diffraction by Rocket Exhausts
NTIS | 1967
|Spacecraft contamination from rocket exhausts
AIAA | 1981
|Chemistry of lonization in Rocket Exhausts
AIAA | 1963
|Causes of ionization in rocket exhausts
AIAA | 1975
|Radar attenuation in solid propellant rocket exhausts
NTRS | 1962
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