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

7th International Scientific and Research Conference "Topical Issues in Aeronautics and Astronautics"

航空航天工程

Ustinov, L.A.^1 ; Zelenkov, P.V.^2 ; Kovalev, I.V.^2

TULA STAT UNIVERSINY, Tula

300012, Russia^1

Reshetnev Siberian State Aerospace University, Krasnoyarsk, 660037, Russia^2

关键词: Firing ranges;    Optimal choice;    Trajectory optimization;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/155/1/012040/pdf
DOI  :  10.1088/1757-899X/155/1/012040

学科分类：航空航天科学

来源: IOP

【 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.