FIELD: space engineering. SUBSTANCE: proposed method includes injection of spacecraft with high-thrust engine into initial elliptical orbit at perigee altitude below altitude of geostationary orbit , apogee altitude above altitude of geostationary orbit and inclination of orbit plane different from inclination of geostationary orbit. Magnitudes of angular sectors of operation of low-thrust engines in apogee and perigee areas and maximum angle of deflection of thrust vector by yawing are selected to be constant at entire stage of injection. Apogee altitude is determined from the following formula: 
where i is inclination of transfer high-elliptical orbit. EFFECT: minimization of injection time and cost. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF INJECTION OF SPACECRAFT INTO PRESET ORBIT BY MEANS OF THRUSTERS | 2001 |
|
RU2208557C1 |
| METHOD FOR MOVING SPACECRAFT TO GEOSTATIONARY ORBIT USING LOW-THRUST ENGINES | 2014 |
|
RU2586945C2 |
| METHOD OF THE GEOSTATIONARY REGION SURVEY FOR THE SPACE DEBRIS ELEMENTS AND OTHER OBJECTS OBSERVATION FROM SPACE CRAFT ON THE SEMI-DIURNAL HIGH-ELLIPTIC ORBIT | 2017 |
|
RU2659379C1 |
| METHOD OF CONTROLLING SPACE VEHICLE DURING FLIGHT OF SPACECRAFT FROM ORBIT OF THE MOON TO THE EARTH'S ORBIT | 2019 |
|
RU2725091C1 |
| METHOD OF CONTROLLING ACTIVE FLIGHT OF SPACE OBJECT TO BE DOCKED WITH PASSIVE SPACESHIP | 2010 |
|
RU2440281C1 |
| METHOD OF TRANSPORT SPACE SYSTEM CONTROLLING | 2015 |
|
RU2605463C2 |
| METHOD OF LAUNCHING SPACECRAFTS INTO GEOSTATIONATY ORBIT USING ELECTRIC PROPULSION ENGINES | 2015 |
|
RU2619486C2 |
| METHOD FOR COLLOCATION WHEN TRANSFERRING A GEOSTATIONARY SPACE VEHICLE TO ANOTHER OBSERVATION LONGITUDE AND REMOVING TO A BURIAL ORBIT | 2022 |
|
RU2786680C1 |
| SPACECRAFT WITH LOW-THRUST ENGINE PLANT | 2001 |
|
RU2223893C2 |
| METHOD FOR SIMULTANEOUSLY PUTTING GROUP OF SATELLITES INTO NON-COPLANAR ORBITS (VERSIONS) | 2015 |
|
RU2583507C1 |
