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Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS
1 1., 1 1., 1 1., 1 1., 1 1.
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.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
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.
Assessment of a liquid rocket engine concept based on innovative technologies
Solodovnikov A.V., Akinshin I.A., Golubyatnik V.V., Krivonogov A.V.
Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N
Nigodjuk V.E., Sulinov A.V.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
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.
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.
Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants
Nigodjuk V.E., Sulinov A.V.
1 - 13 of 13 Items

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