FIELD: transport.
SUBSTANCE: invention relates to space cable systems (SCS) and can be used for the transfer of SCS to a spinning mode in the orbit plane without the application of jet engines. SCS development is executed from its initial compact state in the circular orbit by the repulsion of objects at a low relative speed. SCS end weights are connected by a cable, its length being varied by a cable feed-haul-in device arranged on one of the end objects. The objects are separated by a vector of local peripheral speed, for example, by a pusher. The objects are driven by a start pulse to separate the objects in practically free paths at the free feed of the cable. The cable development is terminated by the SCS transfer to a stable mode of associated pendulum motion at the stretched preset-length cable. At a definite range of angular phases of this mode the SCS objects are stretched by hauling in the cable at a definite constant speed. This results in changing the SCS into the spinning mode at a preset power integral and fixed final end of the cable.
EFFECT: relaxed weight-size constrictions of SCS, enhanced performances.
8 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF MANOEUVRING DEVIATION OF SPACECRAFT ON ORBIT FROM COLLISION WITH OTHER BODIES | 2015 |
|
RU2586920C1 |
METHOD OF DELIVERY OF LANDER FROM ORBITAL STATION TO EARTH BASED ON PASSIVE DEPLOYMENT OF SPACE CABLE SYSTEM | 2011 |
|
RU2497729C2 |
DEPLOYMENT OF SPACE ROPE SYSTEM AT DELIVERY OF LANDER FROM ORBITAL STATION TO GROUND | 2014 |
|
RU2564930C1 |
METHOD OF UNIAXIAL ORIENTATION OF ELONGATED SPACE VEHICLE | 2010 |
|
RU2457159C2 |
METHOD FOR SPACE VEHICLE WITH FIXED PANELS OF SOLAR BATTERIES ORIENTATION CONTROL DURING EXPERIMENTS ON ORBITS WITH MAXIMUM ECLIPSE PERIOD | 2010 |
|
RU2457158C2 |
METHOD OF SPACE REFUSE WITHDRAWAL FROM PAYLOAD ORBIT EXPLOITING CARRIER ROCKET SEPARATED PART AND ACCELERATING UNIT, AND DEVICE TO THIS END | 2010 |
|
RU2462399C2 |
METHOD OF ADAPTIVE CONTROL OVER DISPLACEMENT OF CENTRE OF GRAVITY OF SPACECRAFT | 2011 |
|
RU2487823C1 |
METHOD OF FORMING DUST FLOW FOR MECHANICAL INTERACTION WITH ORBITAL SPACE OBJECTS | 2023 |
|
RU2816322C1 |
METHOD OF HOLDING SPACECRAFT IN GEOSYNCHRONOUS 24-HOUR ORBIT | 2013 |
|
RU2535353C2 |
DEVICE OF STABILIZATION OF ELECTRODYNAMIC CABLE SYSTEM FOR REMOVING SPACE WASTE | 2017 |
|
RU2666610C1 |
Authors
Dates
2014-12-27—Published
2012-07-27—Filed