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Parametric study of lunar landing techniques using a predetermined thrust orientationParametric study of variation in trajectory parameters for predetermined thrust orientation angle to perform lunar descent from parking orbit
Document ID
19650018399
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harlin, S. H., Jr.
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-61075
Report Number: NASA-CR-61075
Accession Number
65N28000
Funding Number(s)
CONTRACT_GRANT: NAS8-20073
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LUNAR ORBIT
DESCENT TRAJECTORY
TRAJECTORY ANALYSIS
THRUST

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