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

Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(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

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

Silyutin M.V., Shustov S.A.

(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 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.

(Rus)

Vol 15, No 4 (2016)

Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine

Semkin Y.V.

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

Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel

Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.

(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 15, No 4 (2016)

Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen

Zubanov V.M., Shabliy L.S., Stepanov D.V.

(Rus)

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

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 18, No 2 (2019)

Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

Ryzhkov V.V., Morozov I.I.

(Rus)

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

Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency

Ageenko Y.I., Ilyin R.V., Pegin I.V.

(Rus)

Vol 17, No 4 (2018)

Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers

Semkin E.V.

(Rus)

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

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.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 17, No 4 (2018)

Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster

Salich V.L.

(Rus)

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

Modeling of intrachamber processes in an oxygen-hydrogen thruster

Vaulin S.D., Salich V.L.

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

Development of thruster chamber operating on oxygen-hydrogen fuel

Salich V.L.

(Rus)

1 - 23 of 23 Items

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