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Optimum thrust-limited orbit transfer in strong gravity fieldsMinimum time low thrust rocket transfer between elliptic orbits in strong gravity field, using averaging method
Document ID
19710048119
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edelbaum, T. N.
Date Acquired
August 6, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: SPRINGER-VERLAG,
Subject Category
Space Sciences
Meeting Information
Meeting: SYMPOSIUM ON OPTIMIZATION
Location: NICE
Country: FRANCE
Start Date: June 29, 1969
End Date: July 5, 1969
Sponsors: INTERNATIONAL FEDERATION FOR INFORMATION PROCESSING
Accession Number
71A28816
Funding Number(s)
CONTRACT_GRANT: NASW-1684
Distribution Limits
Public
Copyright
Other

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