FIELD: space equipment. SUBSTANCE: positioning of attachment units of nose fairing on pressure hull of orbital spacecraft as well as special design of frame increasing density of packing makes it possible to enhance useful load of orbital spacecraft. EFFECT: enhanced useful load of spacecraft. 5 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2072954C1 |
| STAGE OF LAUNCH VEHICLE FOR INJECTION OF SPACE VEHICLE | 1992 |
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| ROCKET COMPARTMENT-PLATFORM FOR ATTACHMENT OF PAYLOAD COMPONENTS | 1993 |
|
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|
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| MULTI-STAGE MISSILE | 1993 |
|
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| ROCKET FOR SPACE MISSION | 1992 |
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| METHOD OF LAUNCHING MULTI-STAGE SPACE LAUNCH VEHICLE BY MEANS OF CARRIER-AIRCRAFT AND MULTI-STAGE SPACE LAUNCH VEHICLE FOR REALIZATION OF THIS METHOD | 2005 |
|
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| METHOD OF DELIVERY OF PAYLOAD BY SOLID-PROPELLANT ROCKET TO NEAR-EARTH ORBIT AND SOLID-PROPELLANT ROCKET USED FOR REALIZATION OF THIS METHOD | 1993 |
|
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| STAGE OF FLIGHT VEHICLE | 1992 |
|
RU2021581C1 |
| METHOD OF INJECTION OF USEFUL LOAD INTO NEAR SPACE | 1994 |
|
RU2078010C1 |
