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An application of the method of matched asymptotic expansions to ordinary and optimal problems in hypervelocity flight dynamicsMatched asymptotic expansion method applied to ordinary and optimal trajectory problems in hypervelocity flight dynamics
Document ID
19670017072
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Willes, R. E.
(PH. D. THESIS)
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-84105
TE-14
Report Number: NASA-CR-84105
Report Number: TE-14
Accession Number
67N26401
Funding Number(s)
CONTRACT_GRANT: NSG-254-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SERIES EXPANSION
ASYMPTOTIC FUNCTION
TRAJECTORY ANALYSIS
FLIGHT OPTIMIZATION
HYPERVELOCITY
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