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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.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Experimental development of the LRE with CCCM nozzle’s extension
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Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
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.
Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants
Nigodjuk V.E., Sulinov A.V.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
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.
Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup
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1 - 12 of 12 Items

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