Pesquisa

Edição
Título
Autores
HYDRODYNAMIC INSTABILITY AT CAVITATIONAL OPERATING MODES OF HIGH-SPEED PUMPS
Krayev M.
To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines
Dubynin P., Tolstopyatov M., Zuev A., Chernenko V.
ACCELERATED UNWINDING OF THE ROTOR BOOSTER PUMP OF LIQUID ROCKET ENGINES UNDER START-UP CONDITIONS
Belayev E., Vorobyev A.
ABOUT LEGITIMACY OF USAGE OF AGREED PROBABILITIESOF FAILURE-FREE WORK AND AGREED BREAKDOWNS PROBABILITIESDENSITIES IN AGGREGATES RELIABILITY MATHEMATICAL MODELS
Boyko O., Boyko O.
INCREASE OF CAVITATING QUALITIES OF THE PUMP UNITOF THE LIQUID ROCKET ENGINE IN MODE OF SUPPLYOF CRYOGENIC COMPONENTS OF ENGINE FUEL
Kraeva E., Kraev M., Pekarskiy A., Кraeva E., Кraev M., Pecarski A.
Concentration of carbon dioxide in products of combustion of GTE NK-16ST and NK-16-18ST
Baklanov A.
“VIRTUAL CC&RP” - A MATHEMATICAL MODEL FOR THE CONTROL OF THE UNIT CC&RP AND ITS VISUALIZATION WITH THE HELP OF SOFTWARE PRODUCTS WinCC 7.0 AND Step 7
Piskazhova T., Sidelnikov S., Belolipetskii V., Yakivyuk P., Sidelnikov A.
Heat transfer in the centrifugal force field for gas turbines elements
Zuev A., Arngold A., Khodenkova E.
Some units spacecraft balancing
Krushenko G., Golovanova V.
Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function
Torgashin A., Zhujkov D., Nazarov V., Begishev A.
INFLUENCE OF LAUNCH PARAMETERS OF LIQUID ROCKET ENGINE ON THE BALANCE OF AXIAL FORCES IN THE TURBOPUMP
Belayev E., Vorobyev A.
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
INCREASE OF THE PURITY OF METAL PRODUCTS SURFACES WITH APPLICATION OF NANOTECHNOLOGIES
Krushenko G.
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