For citations:
Kirshina A.A., Levikhin A.A., Kirshin A.Yu. Numerical method for calculating the nozzle thrust of a wide-range rocket engine. Scientific and Technical Journal of Information Technologies, Mechanics and Optics. 2022;22(5):1016-1024. (In Russ.) https://doi.org/10.17586/2226-1494-2022-22-5-1016-1024