| 摘要 |
FIELD: space engineering. SUBSTANCE: proposed method includes injection of spacecraft by high-thrust engines into initial elliptical orbit at perigee altitude below perigee altitude of preset orbit, apogee altitude above apogee altitude of preset orbit and inclination of plane of orbit another as inclination of preset orbit; it includes deceleration sections in area of perigee and acceleration sections at change of inclination of orbit is area of apogee; angular sectors of operation of thrusters in area of apogee and perigee and maximum angle of deflection of thrust vector in yawing are selected constant during entire period of injection. EFFECT: facilitated procedure; lost cost. 1 dwg |
