FIELD: rocket technology.
SUBSTANCE: invention relates to rocket technology, namely to connecting devices for multi-stage rockets, disconnection means. A device for removal of a protective sleeve from a warhead (hereinafter – WH) under water consists of WH, a protective sleeve, which is fixed on WH with a stopper, a piston, fuses, and a groove. Inside the protective sleeve, there is a cup in the form of a tube, inside which WH is placed and fixed to the protective sleeve with the stopper. A groove is made on the cup. Inside the cup, a piston with rubber membrane is placed, made in the form of a nose part of WH. From the end of the protective sleeve, a gas generator with a combustion chamber and a fuse is installed. All fuses, by means of an electric bundle, are connected to a control unit located in a sealed volume between the cup and the protective sleeve.
EFFECT: increase in the reliability of removal of a protective sleeve from a warhead under water.
1 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE | 2008 |
|
RU2370726C1 |
| GUIDED MISSILE | 2008 |
|
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| GUIDED SHELL | 2007 |
|
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| GUIDED MISSILE | 2007 |
|
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| BALLISTIC CAP OF ARTILLERY GUIDED MISSILE | 1995 |
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| METHOD FOR SEPARATION OF BALLISTIC CAP OF GUIDED MISSILE AND BALLISTIC CAP FOR ITS REALIZATION | 2004 |
|
RU2246690C1 |
