FIELD: weapons.
SUBSTANCE: invention relates to missiles and can be used in small-size missiles with jettisonable booster. Proposed missile incorporates jettisonable booster with engine, sustainer arranged in adapter bulkhead attached on the engine, gas generator and piston. The said sustainer is locked by blow-out elements, its housing being made with tapered thickening towards rear end face. Piston representing asymmetric convex plate is arranged between the sustainer and gas generator to move jointly with the former in separation of missile stages. Aforesaid piston is locked by split ring, partially deepened into gas generator and fastened on adapter bulkhead. Note that a sleeve is arranged between gas generator and engine.
EFFECT: simpler design and higher reliability.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET | 2018 |
|
RU2690987C1 |
| MISSILE AND DRIVE OF MISSILE STAGE SEPARATION MECHANISM | 2005 |
|
RU2284460C1 |
| ROCKET | 2016 |
|
RU2613391C1 |
| MISSILE | 2005 |
|
RU2284457C1 |
| MISSILE AND GAS GENERATOR OF MISSILE STAGE SEPARATION MECHANISM | 2005 |
|
RU2284456C1 |
| ROCKET | 2008 |
|
RU2362113C1 |
| MISSILE | 2011 |
|
RU2460965C1 |
| ROCKET | 2017 |
|
RU2660968C1 |
| ROCKET | 2002 |
|
RU2202761C1 |
| ROCKET | 2009 |
|
RU2399867C1 |
