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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.
Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling
Vorobiev A.G., Borovik I.N., Ha S.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Particularity of thermal condition computation oF LRE with cooling by liquid oxygen
1 1.
Development of intelligent peripheral devices of control and emergency protection systems for ground testing of liquid-propellant rocket engines
Volnukhin O.A., Liseykin V.A., Tozhokin I.A., Churin M.N.
CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine
Zubanov V.M., Shabliy L.S.
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.
Creation of the technique of he delivery influence on working process in the LRE chamber with expulsion propellant supply
Shnyakin V.N., Kovalenko A.N., Kovalenko V.N., Rod'kin A.V., Bochev E.N., Makoter A.P., Blishun Y.V.
Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets
Vorobiev A.G., Borovik I.N., Ha S.
1 - 11 of 11 Items

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