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Optimal three dimensional reentry trajectories for Apollo-type vehiclesNumerical optimization method based on perturbation theory for calculating optimal three dimensional reentry trajectories for Apollo type vehicles
Document ID
19700030196
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williamson, W. E., Jr. (Texas Center for Research Austin, TX, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-108649
Report Number: NASA-CR-108649
Accession Number
70N39512
Funding Number(s)
CONTRACT_GRANT: NAS9-9903
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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