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卷 24, 编号 4 (2023)
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
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(Rus) PDF
(Eng)
卷 23, 编号 4 (2022)
Methodology for assessing reliability of stand-bed systems in testing liquid throat engines
Nazarov V., Piunov V., Kolomentsev A., Yatsunenko V., Golikovskaya K.
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(Rus)
卷 21, 编号 1 (2020)
Features and modernization methods of thrust measurement devices for liquid rocket engine test stands
Begishev A., Zhuravlev V., Torgashin A.
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(Eng)
卷 21, 编号 3 (2020)
Study of impeller design parameters effect on the axial thrust of a centrifugal electric pump assembly
Kuznetsova Z., Sinichenko M., Kuznetsov A., Kleshnina I., Sin'kovskiy F.
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(Eng)
卷 22, 编号 2 (2021)
Characteristics of low thrust liquid-propellant rocket engines testing process
Nazarov V., Piunov V., Yatsunenko V., Savchin D.
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(Rus) PDF
(Eng)
卷 23, 编号 3 (2022)
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
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(Rus)
卷 22, 编号 2 (2021)
Conversion use of models of working processes of rocket engine turbine installations in the application to local power engineering
Abroskin V., Chernorot V., Kishkin A., Delkov A., Zhuravlev V.
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(Rus) PDF
(Eng)
卷 12, 编号 2 (2011)
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y., Yermoshkin Y.
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(Rus)
卷 12, 编号 4 (2011)
DEVELOPING LRE OF LOW THRUST USING PROPELLANTS : STRONG HYDROGEN PEROXIDE WITH KEROSENE
Vorobiev A., Borovik I., Ha S.
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(Rus)
卷 17, 编号 4 (2016)
The Method of CALCULATION OF THERMAL STATE OF CHAMBER FOR steady state IMPULSE operation OF LIQUID ROCKET ENGINE OF SMALL THRUST
Vorobyev A., Vorobyeva S.
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