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
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|
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LOCK-PUSHER | 1991 |
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INTERORBITAL TOWING VEHICLE | 1995 |
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TANK | 1993 |
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Authors
Dates
1998-04-27—Published
1990-04-20—Filed