NASA NTRS · 19670000479
Fortran 4 program for two-impulse rendezvous analysis
Abstract
Program 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.
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Barling, W. H., Jr., Brothers, W. J., Darling, W. H., Jr.. 1967-12-01. Fortran 4 program for two-impulse rendezvous analysis. https://ntrs.nasa.gov/citations/19670000479
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