Gorelov's solution for maximum time of active flight in horizontal plane at given finite mass is applied to particular problem where thrust applied during some parts of trajectory is used solely for sustaining constant altitude of flight.
On problem of optimum rocket trajectories
K zadache ob optimal'nykh traektoriyakh rakety
Prikladnaya Matematika i Mekhanika ; 28 , n 2
1964
2 pages
Aufsatz (Zeitschrift)
Russisch
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