NASA NTRS · 19670021353
The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude
Abstract
Impulsive solution used to solve optimum trajectory problems with bounded thrust magnitude
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Jezewski, D. J.. 1967-07-01. The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude. https://ntrs.nasa.gov/citations/19670021353
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