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Selection of Optimal Trajectories of Spacecraft Launch Vehicles Authors: Kompaniyets E. Hong Kong 3 Vietnam Da Nang;Thanh H?a 2 Ukraine Dnipro; Dnipro 2 China Pekin; 2 Netherlands Amsterdam; Amsterdam 2 Finland Helsinki 1 Argentina Bragado 1 France Paris 1 Spain Madrid 1 Latvia Riga 1 Romania Voluntari 1 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Kompaniyets E. Kompaniyets E. Selection of Optimal Trajectories of Spacecraft Launch Vehicles Автори: Kompaniyets E. Selection of Optimal Trajectories of Spacecraft Launch Vehicles Автори: Kompaniyets E. Selection of Optimal Trajectories of Spacecraft Launch Vehicles Автори: Kompaniyets E. Selection of Optimal Trajectories of Spacecraft Launch Vehicles Автори: Kompaniyets E.
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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
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