المؤلفون: Bogatiy, Aleksander V.^Aff7, Dyakonov, Grigory A.^Aff7, Elnikov, Roman V.^Aff7, Popov, Garri A.^Aff7

المساهمون: Howlett, Robert J., Series Editor^Aff1, Jain, Lakhmi C., Series Editor^{Aff2, Aff3}, Favorskaya, Margarita N., editor^Aff4, Nikitin, Ilia S., editor^Aff5, Reviznikov, Dmitry L., editor^Aff6

المصدر: Applied Mathematics and Computational Mechanics for Smart Applications : Proceedings of AMMAI 2020. 217:141-154

المؤلفون: V. V. Ryzhkov, A. V. Sulinov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 4, Pp 115-128 (2018)

مصطلحات موضوعية: small and ultra-small spacecraft, propulsion systems, low-thrust rocket engines operating on various physical principles, total thrust impulse, specific thrust impulse, thrust, electric energy consumption, propulsion-system mass, spacecraft mass, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://journals.ssau.ru/vestnik/article/viewFile/6385/6266; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533

URL الوصول: https://doaj.org/article/591e0e16dc6e4221b13142d7a62746ca

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