FIELD: mechanical engineering. SUBSTANCE: device has load- bearing structure and separation charges connecting the load-bearing structure with rocket case. Load-bearing structure is provided with at least three supports made in form of plates with bearing members made in form of cone or sphere engageable with mating mount seat provided in rocket case and with tensioner. Load-bearing structure is connected with rocket case by means of separation charge mounted symmetrically relative to supports; tensioner is made in form of turnbuckles connecting the load-bearing structure with separation charge. EFFECT: enhanced reliability. 3 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
HATCH COVER OF THERMOSTATIC CONTROL SYSTEM | 1995 |
|
RU2094308C1 |
ROCKET INSTRUMENTATION SECTION | 1994 |
|
RU2089473C1 |
DEVICE FRO BREAKAWAY INTERUNIT CABLE JOINT OF ROCKET | 1994 |
|
RU2093775C1 |
LARGE-SIZE SPACE COLLAPSIBLE REFLECTOR | 1996 |
|
RU2101811C1 |
ASTRONAUT BERTH | 1993 |
|
RU2089470C1 |
CRYOGENIC STAGE | 1996 |
|
RU2105702C1 |
ROCKET POD | 1996 |
|
RU2095294C1 |
CAPACITIVE LEVEL GAUGE | 1996 |
|
RU2112931C1 |
MULTI-UNION DETACHABLE UNIT | 1998 |
|
RU2137016C1 |
HYDRAULIC DRIVE | 1996 |
|
RU2103564C1 |
Authors
Dates
1997-07-10—Published
1993-06-01—Filed