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
01.10.1972
Sonstige
Keine Angabe
Englisch
Study of high altitude plume impingement
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