3. Selection of Optimal Trajectories of Spacecraft Launch Vehicles
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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 |
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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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