FIELD: rocket technology.
SUBSTANCE: invention relates to rocket technology and concerns housings of guided missile compartments. The rocket compartment body is made detachable into two halves (1) and (2) along a plane aligned with the longitudinal axis of the rocket. The connecting fasteners are arranged radially in the housing. When bolts (4) are installed, nuts (3) are held in joint by the structure of body halves (1) and (2).
EFFECT: strength and reliability of the longitudinal joint is ensured using standard fasteners with no effect of fasteners on the aerodynamics of the rocket, maintaining the internal volume to accommodate the payload and no need to manufacture a special tool for installing fasteners.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BODY OF THE INSTRUMENT UNIT OF A MISSILE | 2021 |
|
RU2769033C1 |
| LAUNCH VEHICLE OF COMBINED CONFIGURATION | 2000 |
|
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|
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|
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| ROCKET COMPARTMENTS JOINT | 1997 |
|
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| JOINT OF FLIGHT VEHICLE BODY TO BOTTOM | 2002 |
|
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|
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| FASTENING CONNECTION | 2011 |
|
RU2485363C1 |
| ROCKET AND METHOD FOR ITS ASSEMBLY | 1999 |
|
RU2158410C1 |
| DEVICE FOR ATTACHMENT AND SEPARATION OF CLUSTER-CONFIGURATION CARRIER ROCKET | 2012 |
|
RU2521888C1 |
