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Title
Authors
Vol 11, No 3-1 (2012): Special Issue
Interaction of exhaust jets of rocker propulsions on various propellants with atmosphere for estimation of ecological safety of firing of rockets and launchers
Zavelevich F.S., Ushakov N.N.
PDF
(Rus)
Vol 9, No 4 (2010)
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
PDF
(Rus)
Vol 18, No 4 (2019)
Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems
Ryzhkov V.V., Morozov I.I., Lapshin E.A.
PDF
(Rus)
Vol 16, No 2 (2017)
Assessment of a liquid rocket engine concept based on innovative technologies
Solodovnikov A.V., Akinshin I.A., Golubyatnik V.V., Krivonogov A.V.
PDF
(Rus)
Vol 21, No 1 (2022)
On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers
Maksimov A.D., Shustov S.A.
PDF
(Rus)
Vol 20, No 4 (2021)
The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies
Ryzhkov V.V.
PDF
(Rus)
Vol 17, No 4 (2018)
Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft
Ryzhkov V.V., Sulinov A.V.
PDF
(Rus)
Vol 15, No 4 (2016)
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
PDF
(Rus)
Vol 11, No 3-3 (2012): Special Issue
On a method of practical training fulfillment for course of studies “Design of Main Units and Systems of Engine”
Borisov V.A., Zhizhkin A.M.
PDF
(Rus)
Vol 8, No 3-3 (2009): Special Issue
About the centre of science-educational of laser systems and technologies at faculty DLA SSAU
1 1., 1 1., 1 1.
PDF
(Rus)
Vol 19, No 1 (2020)
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
PDF
(Rus)
Vol 17, No 3 (2018)
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
PDF
(Rus)
1 - 12 of 12 Items

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