Relation optimization of the starting and main stages of rockets with short-running engine on the external oxidizer

[摘要] The paper considers an optimal choice of the mass relation of the starting and main stages of the rocket with a short-running engine on the external oxidizer from the point of view of achieving the maximum firing range.

[发布机构] TULA STAT UNIVERSINY, Tula; 300012, Russia^1;Reshetnev Siberian State Aerospace University, Krasnoyarsk, 660037, Russia^2

[学科分类] 航空航天科学

[关键词] Firing ranges;Optimal choice;Trajectory optimization