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New procedure for determining minimum time orbit transfersComputer program includes time minimizing function required for propellant constrained minimum time impulsive transfer between coplanar circular orbits or unrestricted orbits. Basic formulation is extended to include inclined circular or inclined elliptic orbits.
Document ID
19710000374
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Davis, D. A. (BOEING CO.)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-14804
Report Number: MFS-14804
Accession Number
71B10376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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