NASA NTRS · 19660034737
Optimization of step rockets by the discrete maximum principle.
Abstract
Optimum stage weight distribution in multistage rocket obtained by discrete maximum principle
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Fan, L.-T., Hwang, C.-L., Wang, C.-S.. 1965-11-01. Optimization of step rockets by the discrete maximum principle.. https://ntrs.nasa.gov/citations/19660034737
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