Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines

Autor: V. V. Ryzhkov, I. I. Morozov

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

The paper presents the results of calculating thermodynamic and thermophysical properties of the combustion products of gaseous oxygen-hydrogen fuel according to the ideal LRE model taking into account the phase state of the components, as well as th

Externí odkaz: https://doaj.org/article/0dcacf7bb20c4353a40ba4e37a4a4c0d