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3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles

Authors:

Kompaniyets E. P.1, Dron’ M. M.2, Baranov E. Y.1, Litvin M. G.1

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.

Key words:

Bibliography:

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3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles
3.2.2016 Selection of Optimal Trajectories of Spacecraft Launch Vehicles
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