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AN APPLICATION OF A SUCCESSIVE APPROXIMATION SCHEME TO OPTIMIZING VERY LOW-THRUST TRAJECTORIESSpacecraft guidance - low thrust propulsion trajectories
Document ID
19630006928
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pinkham, G. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Date Acquired
August 1, 2013
Publication Date
February 6, 1963
Subject Category
Space Radiation
Accession Number
63N16804
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY
LOW THRUST PROPULSION
SPACECRAFT GUIDANCE
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IDRelationTitle19630006925Collected WorksProgress Report No. 3 on Studies in the Fields of Space Flight and Guidance Theory
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