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An approach to the problem of optimizing orbital maneuversProblem of time open maneuvering of orbital vehicle in Newtonian gravitational field while conserving characteristic velocity of maneuver
Document ID
19670013942
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Busemann, A. (Colorado Univ. Boulder, CO, United States)
Culp, R. D. (Colorado Univ. Boulder, CO, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-83544
Report Number: NASA-CR-83544
Accession Number
67N23271
Funding Number(s)
CONTRACT_GRANT: NGR-06-003-033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT MANEUVER
GRAVITATIONAL FIELD
ORBIT

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