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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 23, No 3 (2024)

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

Musteikis A.I., Levikhin A.A., Kolosenok S.V.

(Rus)

Vol 23, No 1 (2024)

Optimization of trajectory motion of the first stage of an aerospace system

Khramov A.A.

(Rus)

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 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(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 3-4 (2011): Special Issue

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

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

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

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

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(Rus)

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

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

Vol 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

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

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.

(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 3-3 (2011): Special Issue

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

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

Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered

1 1.

(Rus)

Vol 9, No 2 (2010): Special Issue

Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust

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

(Rus)

Vol 16, No 3 (2017)

Locally optimal control of space tug motion between the libration points of the Earth-Moon system

Starinova O.L., Fain M.K.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(Rus)

1 - 20 of 20 Items

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