FIELD: aviation.
SUBSTANCE: group of inventions relates to means and methods of launch, orbit and de-orbit automatic payloads (PL) using unmanned rocket and space complex (RSC). The RSC includes an upper stage (US) with control devices for the launch vehicle, which, when separating PL from the US, remotely control the service systems of PL, the fuel reserve for PL disengagement, the docking system with PL in the working orbit and the manipulator for maintenance and installation of PL on US. PL can be performed and inseparable from US. LF or remote control of the PL, after its separation, the US is moved to the specified place of the orbit. The power supply of PL is carried out with the use of equipment delivered by US or from standard airborne systems of US. The PL deorbit is carried out with the help of US, after its rapprochement and docking with it.
EFFECT: minimization of control and power systems of the rocket and space complex, simplification of the process of launching into orbit, the possibility of complete subsequent utilisation of the components of rocket and space complex.
2 cl, 4 dwg
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|---|---|---|---|
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|
RU2666014C1 |
| METHOD OF SPACE REFUSE WITHDRAWAL FROM PAYLOAD ORBIT EXPLOITING CARRIER ROCKET SEPARATED PART AND ACCELERATING UNIT, AND DEVICE TO THIS END | 2010 |
|
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|
RU2265558C1 |
| SPACE ROCKET SYSTEM AND METHOD FOR RENDERING SERVICES IN LAUNCHING SPACE VEHICLES USING SPACE ROCKET SYSTEM | 2001 |
|
RU2179941C1 |
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|
RU2811792C1 |
| MULTI-STAGE SPACE LAUNCH VEHICLE | 2005 |
|
RU2265560C1 |
| METHOD OF MANAGING THE MOVEMENT OF COMPLEX FORMATION OF THE SPACE APPARATUS GROUP | 2017 |
|
RU2683700C1 |
| METHOD FOR CONDUCTING FLIGHT DEVELOPMENT TESTS OF AUTONOMOUS DOCKING MODULE FOR CLEANING ORBITS FROM SPACE DEBRIS | 2016 |
|
RU2643020C1 |
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|
RU2254265C9 |
