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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.
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.
Backgrounds and trends of all-electric propulsion geostationary satellites creation
Vnukov A., Rvacheva E.
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.
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A., Vnukov A., Balandina T., Balandin E., Tarletskiy I.
LOW-POWER RADIO-FREQUENCY ION THRUSTER
Akhmetzhanov R., Bogatyi A., Dronov P., Dyakonov G., Ivanov A.
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.
Geo satellite attitude and orbit control: fixed orbit control thrasters
Ermoshkin Y., Raevsky V., Urusov V.
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.
GEOSTATIONARY SPACECRAFT ATTITUDE AND ORBIT CONTROL BY MOTIONLESS ORBIT CONTROL THRUSTERS
Yermoshkin Y., Raevsky V., Urusov V.
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yermoshkin Y., Volkov D., Yakimov E.
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.
Electric propulsions rational application range on the applied spacecrafts
Ermoshkin Y., Yermoshkin Y.
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.
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y., Urusov V., Yermoshkin Y., Urusov V.
Electric power supply of heater elements of electric propulsion thruster by regulated alternating current
Moshnyakov A., Mikhaylov M.
GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y., Raevskiy V., Urusov V., Yermoshkin Y., Raevsky V., Urusov V.
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