FIELD: rocketry and space engineering; flying vehicles including satellite with attached structures (solar batteries). SUBSTANCE: flying vehicle has case on which swivel attached structures are mounted with attachment units located beyond satellite. Flying vehicle is also provided with adapter and retainers connecting the satellite with rocket and separating them in accordance with flight program. Attachment units of attached structure are located on adapter. When surface jobs are conducted, satellite with attached structures is coupled with adapter. Upon completion of injection of satellite by launch vehicle, adapter is uncoupled from satellite and is left on rocket. EFFECT: enhanced efficiency and low cost. 2 cl, 3 dwg
Title | Year | Author | Number |
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SPACECRAFT UNDOCKING SYSTEM | 2012 |
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RU2514981C2 |
SOLAR BATTERY PANEL | 1999 |
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LAUNCH VEHICLE STAGE FOR FLIGHT-DESIGN TESTS | 2002 |
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METHOD AND DEVICE FOR HOLDING OBJECTS | 1993 |
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SPACECRAFT TEMPERATURE CONTROL SYSTEM | 1999 |
|
RU2151722C1 |
METHOD OF DEPLOYMENT OF MULTI-SECTIONAL STRUCTURES AND MULTI-SECTIONAL STRUCTURE USED FOR REALIZATION OF THIS METHOD | 1993 |
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RU2123875C1 |
INSTRUMENTS AND EQUIPMENT SHOCK TEST METHOD | 2002 |
|
RU2234690C2 |
Authors
Dates
2003-02-10—Published
1999-02-08—Filed