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Trajectory optimization for an Apollo-type vehicle under entry conditions encountered during lunar returnTrajectory optimization for Apollo-type vehicle under entry conditions during lunar return
Document ID
19670015714
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Smith, R. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Yound, J. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Space Sciences
Report/Patent Number
NASA-TR-R-258
Accession Number
67N25043
Funding Number(s)
CONTRACT_GRANT: 125-17-05-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY OPTIMIZATION
RETURN-TO-EARTH PHASE
APOLLO SPACECRAFT
SPACECRAFT REENTRY

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