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.
Fortran 4 program for two-impulse rendezvous analysis
1967-12-01
Miscellaneous
No indication
English
Optimal multiple-impulse orbital rendezvous
NTRS | 1967
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