NASA NTRS · 19710051346
An optimal, analytic solution to the linear- gravity, constant-thrust trajectory problem
Abstract
Constant-thrust trajectory problem with gravitational acceleration as linear function of radius vector, obtaining minimum fuel solution in integrals
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Jezewski, D. J.. 1971-07-01. An optimal, analytic solution to the linear- gravity, constant-thrust trajectory problem. https://ntrs.nasa.gov/citations/19710051346
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