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Vol 23, No 2 (2024)

Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles

Ageenko Y.I., Bubnova A.S.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

Vol 22, No 2 (2023)

Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment

Balyakin V.B., Lavrin A.V., Dolgikh D.E.

(Rus)

Vol 18, No 4 (2019)

Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control

Shorikov A.F., Kalev V.I.

(Rus)

Vol 15, No 4 (2016)

Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials

Krivonogov A.V.

(Rus)

Vol 9, No 1 (2010)

Defining the specific impulse of mixed solid propellants

1 1., 1 1.

(Rus)

Vol 18, No 3 (2019)

Disturbed motion of the hypersonic first stage of an aerospace system in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 15, No 4 (2016)

Analysis of low-thrust liquid rocket engines with a methane air pump unit

Ivanov A.I., Kositsin I.P., Borisov V.A.

(Rus)

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

Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation

1 1.

(Rus)

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

Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

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

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

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

Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Iodine as an alternative propellant for electrojet engines

Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.

(Rus)

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

Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 18, No 1 (2019)

Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system

Balakin V.L., Krikunov M.M.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 16, No 2 (2017)

Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines

Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.

(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)

Vol 19, No 2 (2020)

Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

Vol 15, No 4 (2016)

Mathematical modelling of the working process of a hot gas pressure feed system

Salich V.L.

(Rus)

Vol 9, No 2 (2010): Special Issue

Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent

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

(Rus)

1 - 22 of 22 Items

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