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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.
Heat transfer in the centrifugal force field for gas turbines elements
Zuev A., Arngold A., Khodenkova E.
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.
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.
Analysis of electromagnetic processes in ac-dc converters with possibility of reverse flow of energy and increased efficiency
Krasnobaev Y., Zakharov V., Karnaukhov M.
Chemical and kinetic energy storage device
Nadaraia C., Babkina L., Shestakov I., Fadeev A.
PROPULSION OF A SPACECRAFT WITH THE ROTATING BATTERIES
Nadaraia C., Chestakov I., Fadejev A., Nadaraia K.
ANALYSIS OF THE DYNAMIC PERFORMANCE OF THE POINTING AND ATTITUDE CONTROL SUBSYSTEM OF THE RESILIENT SPACECRAFT WITH POWER GYROSCOPIC UNIT ON THE BASIS OF ГД 02-150 GYRODYNE
Yakimov E., Raevskiy V., Lukyanenko M.
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