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Vol 23, No 2 (2024)

Comparative results of computational and theoretical study of the annular nozzle with a flat central body

Kirshina A.A., Levikhin A.A., Kirshin A.Y.

(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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions

Shustov S.A.

(Rus)

Vol 13, No 1 (2014)

Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets

Ivanov I., Kryukov I., Shustov S.

(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.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 9, No 1 (2010)

Defining the specific impulse of mixed solid propellants

1 1., 1 1.

(Rus)

Vol 14, No 1 (2015)

Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine

Dovgjallo A.I., Shimanov A.A.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Influence of impulse generation mode on electro-erosion treatment

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 19, No 1 (2020)

Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem

Lu H., Wang C., Zabolotnov Y.M.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft

Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Firing test stand pulse detonation low-thrust engines

Govorenkho G.S., Teterin D.P., Kotelnikhov D.S., Aliluev A.V., Aliluev S.V., Fedorets V.N.

(Rus)

Vol 18, No 3 (2019)

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.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Formation of the sliding surface mechanical seal different methods

Tarelnik V.B., Martsinkovskiy V.S., Antoshevskiy B.

(Rus)

Vol 8, No 1 (2009)

Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding

Shustov S.A.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices

Shustov S.A.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines

Petrukhin N.V., Sergeev S.M., Prokopenko O.A., Grek M.O.

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters

Beshenev Y.A., Buldashev S.A., Kazankin F.A., Lemskiy N.V., Semkin Y.V.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Design procedure of fundamental parameters of the direct-flow detonation pulsing engine

Porshnev V.A.

(Rus)

Vol 10, No 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(Rus)

1 - 21 of 21 Items

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