3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles
Organization:
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; Oles Honchar Dnipro National University, Dnipro, Ukraine2
Page: Kosm. teh. Raket. vooruž. 2016 (2); 17-29
Language: Russian
Annotation: An analysis of the existing methods of trajectories selection of spacecraft launch vehicles is performed. A generalized method is proposed for selection of optimal flight trajectories of launch vehicles in the central gravitational field when launching the artificial earth satellites.
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