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Trajectory And Heating Of A Hypervelocity ProjectileTechnical paper presents derivation of approximate, closed-form equation for relationship between velocity of projectile and density of atmosphere. Results of calculations based on approximate equation agree well with results from numerical integrations of exact equations of motion. Comparisons of results presented in series of graphs.
Document ID
19920000106
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Tauber, Michael E.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11805
Accession Number
92B10106
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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