المؤلفون: V. V. Ryzhkov, I. I. Morozov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 131-142 (2019)

مصطلحات موضوعية: low-thrust rocket engine, gaseous oxygen-hydrogen fuel, models of the working process (thermodynamic and computational gas dynamics), operation and design factors, engine specific impulse, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://journals.ssau.ru/index.php/vestnik/article/view/7460; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533

URL الوصول: https://doaj.org/article/0dcacf7bb20c4353a40ba4e37a4a4c0d

المؤلفون: V. V. Ryzhkov, I. I. Morozov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 2, Pp 62-74 (2019)

مصطلحات موضوعية: Low-thrust rocket engine, gaseous oxygen-hydrogen fuel, model of the working process, technology of computational analysis, distribution of parameters in the gas-dynamic path, parametric study, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://journals.ssau.ru/index.php/vestnik/article/view/6742; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533

URL الوصول: https://doaj.org/article/b1f46900ffde457ab0e77065dd3c3161

المؤلفون: V. V. Ryzhkov, I. I. Morozov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 3, Pp 103-115 (2018)

مصطلحات موضوعية: low-thrust rocket engines, gaseous oxygen-hydrogen fuel, mixing pattern, design parameters of the working process, combustion products temperature distribution, specific thrust impulse, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://journals.ssau.ru/vestnik/article/viewFile/6333/6215; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533

URL الوصول: https://doaj.org/article/09b6c1493d054128b6873f04fd6dd142