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NASA NTRS · 19630025672

CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION

Abstract

Optimum thrust programming studies include a comparison of constant and variable attitude thrust programs for an earth-mars rendezvous

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BibTeXRIS

Melbourne, W. G., Sauer, C. G., Jr.. 1963-08-21. CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION. https://ntrs.nasa.gov/citations/19630025672

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