FIELD: separation devices of rocket space systems for launching simultaneously two space vehicles by one launch vehicle. SUBSTANCE: separation mechanism is provided with common pressure accumulator mounted on lateral surface of adapter device. EFFECT: enhanced reliability. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET SPACE MODULE | 1990 |
|
RU2109661C1 |
| SELF-CONTAINED ROCKET POD | 1993 |
|
RU2043956C1 |
| POWER PLANT OF SPACECRAFT | 1991 |
|
RU2121071C1 |
| LOCK-PUSHER | 1991 |
|
RU2093435C1 |
| SYSTEM OF TANKAGE | 1996 |
|
RU2092405C1 |
| INTERORBITAL TOWING VEHICLE | 1995 |
|
RU2094331C1 |
| DESCENT VEHICLE FOR LANDING ON SURFACES OF CELESTIAL BODIES HAVING ATMOSPHERE | 1989 |
|
RU2109660C1 |
| TANK | 1993 |
|
RU2042873C1 |
| ROCKET-PROPELLED FLYING VEHICLE (VERSIONS) AND ROCKET ENGINE | 1995 |
|
RU2094333C1 |
| DESCENT VEHICLE | 1992 |
|
RU2057689C1 |
Authors
Dates
1998-04-27—Published
1990-04-20—Filed