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ANALYSIS OF THE REQUIREMENTS PERFERMANCE OF INTERAGANCY COORDINATION COMMITTEE ON DEBRIS PREVENTION
Bulynin Y.L., Sozonova I.L.
Features of the implementation of the satellite communication system in the highly elliptical orbit “Express-RV”
Zharinov V.F., Ponomarev O.G., Bobkov I.V.
GEOSTATIONARY ORBITAL INJECTION OF A SPACECRAFT BY THE COMBINED METHOD
Yakovlev A.V., Vnukov A.A., Balandina T.N., Balandin E.A., Tarletskiy I.S.
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.M., Vnukov A.A., Volkov D.D., Kochev Y.V., Simanov R.S., Yakimov E.N., Grikhin G.S.
The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit
Ermoshkin Y.M., Vnukov A.A., Volkov D.V., Kochev Y.V., Simanov R.S., Yakimov E.N., Pridannikov S.Y.
Optical system of high resolution for Earthimaging from space
Veselkov S.A.
THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION
Finogenov S.L., Kolomentsev A.I.
ECONOMIC METHODS OF SPECTRUM/ORBIT MANAGEMENT FOR SATELLITE NETWORKS
Makarov V.V., Nozdrin V.V.
Study of the payload extraction trajectory heavy class carrier rocket
Bordachev V.A., Kolga V.V.
Perfection of control systems of space vehicles
Krushenko G.G., Golovanova V.V.
ANALYSIS OF CLEANING CONCEPTS OF NEAR-EARTH SPACE
Kirillov V.A., Bagateev I.R., Tarleckiy I.S., Balandina T.N., Balandin E.A.
Spacecraft motion in a low circular orbit in establishing intersatellite link
Kolovsky I.K., Shmakov D.N.
Passage of special sites of the orbit by the navigating space vehicle of system GLONASS
Fateev A.V., Emelyanov D.V., Tentilov U.A., Ovchinnikov A.V.
On the choice of orbits for spacecraft
Egorythev G.P., Shiryaeva T.A., Shlepkin A.K., Filippov K.A., Pashkovskaya O.V.
Near-earth asteroids population
Galushina T.Y.
Determination of the trajectory of motion of celestial bodies in the Earth's atmosphere
Bondarenko J.S., Medvedev Y.D.
Methodological principles of space vehicle design for the maximum energy sup-ply of the payload
Chebotarev V.E., Fatkulin R.F., Vorontsova E.O., Balandina T.N., Shangina E.A.
PROBLEMS OF DEVELOPMENT OF LOW-ORBIT MULTIFUNCTIONAL PERSONAL SATELLITE COMMUNICATION SYSTEM «GONETS-D1M»
Kuzovnikov A.V., Testoedov N.A., Agureev V.A.
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.N., Raevskiy V.A., Lukyanenko M.V.
1 - 19 of 19 Items

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