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Study of high altitude plume impingementComputer 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.
Document ID
19720000600
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wojciechowski, C. J. (Lockheed Missiles and Space Co.)
Penny, M. M. (Lockheed Missiles and Space Co.)
Prozan, R. J. (Lockheed Missiles and Space Co.)
Seymour, D. (Lockheed Missiles and Space Co.)
Greenwood, T. F. (Lockheed Missiles and Space Co.)
Date Acquired
August 6, 2013
Publication Date
October 1, 1972
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-21414
Report Number: MFS-21414
Accession Number
72B10601
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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