FIELD: equipment of space vehicles. SUBSTANCE: method consists in launching the cargo on earth in detachable holders with the aid of electromagnet system and receiving this cargo on earth correcting the moment of throwing by signal of earth beacons. Magnitude of pulse of capsule launching force is brought in synchronism with capsule pressurizing system by means of contacts closed during motion of capsule. EFFECT: simplification of method of delivery of cargo and saving of earth resources. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SPACE LAUNCH AREA | 1998 |
|
RU2131830C1 |
| SOLAR SPACE ORBITAL POWER PLANT | 1994 |
|
RU2094335C1 |
| SOLAR SPACE POWER STATION | 1994 |
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| METHOD OF INTEGRATION OF ORBITAL SPACE COMPLEXES | 1995 |
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| UNIT OF SOLAR SPACE POWER PLANT | 1994 |
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| METHOD OF SPACE ERECTION OF COMPLEX FROM BUILDING BLOCKS IN NEAR-EARTH ORBIT | 1993 |
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| METHOD FOR LAUNCHING OF OBJECT TO SPACE FROM COSMODROME IN SPACE | 2000 |
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RU2241643C2 |
| LEAN-TO FOR SPACE STATION | 1995 |
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| DEVICE FOR DEVELOPMENT OF MOON | 1996 |
|
RU2129077C1 |
| SPACE STATION | 1995 |
|
RU2116942C1 |
