FIELD: rocket and space technology.
SUBSTANCE: invention relates namely to methods for deploying and launching satellites using a mechanical structure on a launch vehicle. The method includes positioning satellites in mounting means spaced apart from each other to prevent collision. Next, the first set of satellites in the axial direction and the second set of satellites in the radial direction are separated. The second set of satellites is divided into two groups. The stage is reoriented and satellites with a low roll rate of 0.20 to 0.35 degrees are separated. The first set of satellites located in the axial direction, a part of the second set of satellites located in the radial direction, and the remaining part of the second set of satellites located at an angle to the said launch vehicle are launched.
EFFECT: it is possible to separate multiple satellites within a short period of time without colliding with each other or with the rocket engine jet with the possibility of video recording.
6 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR DELIVERY OR RETURN OF ARTIFICIAL SATELLITES | 2012 |
|
RU2600971C2 |
| SYSTEM OF INJECTION OF PAYLOAD INTO LOW-ALTITUDE NEAR-EARTH ORBIT | 1997 |
|
RU2191145C2 |
| RECOVERABLE LAUNCH VEHICLE AND MULTIPLE CONFIGURRATION TRANSPORTATIOON SYSTEM | 1991 |
|
RU2035358C1 |
| METHOD FOR LAUNCHING ARTIFICIAL SATELLITES INTO EARTH ORBIT | 2018 |
|
RU2770256C2 |
| SPACE HEAD FOR GROUP LAUNCH OF SATELLITES | 2010 |
|
RU2428358C1 |
| METHOD FOR INJECTION OF SPACE VEHICLES INTO ORBIT | 2023 |
|
RU2794486C1 |
| PAYLOAD LAUNCHING AND TRANSPORTATION SYSTEM | 1999 |
|
RU2233772C2 |
| METHOD FOR SIMULTANEOUSLY PUTTING GROUP OF SATELLITES INTO NON-COPLANAR ORBITS (VERSIONS) | 2015 |
|
RU2583507C1 |
| METHOD FOR SEPARATION OF SATELLITES AND MOVING APART IN ORBIT AT GROUP LAUNCH BY ONE ROCKET | 1994 |
|
RU2111901C1 |
| METHOD FOR SEPARATING PAYLOADS FROM THE ORBITAL STAGE OF THE LAUNCH VEHICLE WITH A LIQUID PROPELLANT ENGINE | 2020 |
|
RU2748079C1 |
