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Some numerical results of geocentric low thrust trajectory optimizationDetermination of optimum, coplanar, circle-to- circle, transfer trajectories for low thrust space vehicles in strong central force field
Document ID
19650023460
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hinz, H. K. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Mc Gill, R. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Taylor, G. (Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Date Acquired
August 2, 2013
Publication Date
July 12, 1965
Subject Category
Space Sciences
Accession Number
65N33061
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY ANALYSIS
LOW THRUST PROPULSION
SPACECRAFT TRAJECTORY
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IDRelationTitle19650023449Collected WorksStudies in the fields of space flight and guidance theory progress report no. 7, 23 jul. 1964 - 1 apr. 196519650023449Collected WorksStudies in the fields of space flight and guidance theory progress report no. 7, 23 jul. 1964 - 1 apr. 1965
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