Computer program has been developed as analytical tool to predict severity of effects of exhaust of rocket engines on adjacent spacecraft surfaces. Program computes forces, moments, pressures, and heating rates on surfaces immersed in or subjected to exhaust plume environments. Predictions will be useful in design of systems where such problems are anticipated.
Study of high altitude plume impingement
1972-10-01
Miscellaneous
No indication
English
Study of high altitude plume impingement
NTRS | 1973
|Study of High Altitude Plume Impingement
NTIS | 1973
|Numerical modeling of transient plume impingement during high altitude rocket staging
British Library Conference Proceedings | 2007
|Space Shuttle Plume and Plume Impingement Study
NTRS | 1977
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