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Volume 22, Nº 3 (2021)
Application of the propulsion subsystem on the base of SPT-100b plasmic thruster to the Express-80 and Express-103 spacecraft’s orbit raising and orbit control
Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Grikhin G.
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(Rus) PDF
(Eng)
Volume 23, Nº 4 (2022)
The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit
Ermoshkin Y., Vnukov A., Volkov D., Kochev Y., Simanov R., Yakimov E., Pridannikov S.
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(Rus)
Volume 15, Nº 4 (2014)
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A., Rvacheva E.
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(Rus)
Volume 22, Nº 1 (2021)
Experimental investigations of a plasma thrusters and its power processing units performances like an electric load of a spacecraft’s power condition system
Ermoshkin Y., Kochev Y., Nikipelov A., Pervukhin A., Simanov R.
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(Rus) PDF
(Eng)
Volume 17, Nº 3 (2016)
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.
Volume 16, Nº 2 (2015)
LOW-POWER RADIO-FREQUENCY ION THRUSTER
Akhmetzhanov R., Bogatyi A., Dronov P., Dyakonov G., Ivanov A.
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(Rus)
Volume 11, Nº 1 (2010)
Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft
Nadiradze A., Shaposhnikov V., Smirnov V., Maximov I., Kochura S.
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(Rus)
Volume 10, Nº 5 (2009)
Geo satellite attitude and orbit control: fixed orbit control thrasters
Ermoshkin Y., Raevsky V., Urusov V.
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(Rus)
Volume 14, Nº 4 (2013)
THE DESIGN OF THE EXPERIMENT AND CREATION OF THE REGRESSION MODEL OF THE SPECIFIC IMPULSE LIQUID ROCKET ENGINE THRUST FROM 10 TO 420 N
Kolomentsev A., Khokhlov A.
PDF
(Rus)
Volume 10, Nº 4 (2009)
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y., Raevsky V., Urusov V.
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(Rus)
Volume 19, Nº 3 (2018)
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y., Volkov D., Yakimov E.
PDF
(Rus)
Volume 13, Nº 1 (2012)
FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS
Nadiradze A., Rachmatullin R., Kochura S., Maksimov I., Smirnov V.
PDF
(Rus)
Volume 12, Nº 2 (2011)
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y., Yermoshkin Y.
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(Rus)
Volume 17, Nº 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.
Volume 12, Nº 1 (2011)
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y., Urusov V., Yermoshkin Y., Urusov V.
PDF
(Rus)
Volume 16, Nº 1 (2015)
Electric power supply of heater elements of electric propulsion thruster by regulated alternating current
Moshnyakov A., Mikhaylov M.
PDF
(Rus)
Volume 11, Nº 4 (2010)
GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y., Raevskiy V., Urusov V., Yermoshkin Y., Raevsky V., Urusov V.
PDF
(Rus)
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