3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles

3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles

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

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

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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