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Fortran 4 program for two-impulse rendezvous analysisProgram determines if rendezvous in near space is possible, and performs an analysis to determine the approximate required values of the magnitude and direction of two thrust applications of the upper stage of a rocket firing. The analysis is performed by using ordinary Keplerian mechanics.
Document ID
19670000479
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Barling, W. H., Jr.
Brothers, W. J.
Darling, W. H., Jr.
Date Acquired
August 3, 2013
Publication Date
December 1, 1967
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-13971
Report Number: MFS-13971
Accession Number
67B10479
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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