FIELD: guided missiles. SUBSTANCE: aft body 3 of the control actuator unit is a truncated cone and forms a closed space with the shaped cavity of the main warhead, that is sealed by corrugated cup 8 with a tapered external surface. Gas generator 9 with an electric primer is installed in the cup cavity. Pipe 11 is secured on body 3 for movement relative to warhead body 12. Installed on the rear part of pipe 11 and front part of body 12 are the guide (13) and retaining members (14,15,16). EFFECT: improved design. 3 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| GUIDED MISSILE | 2007 | 
 | RU2351886C1 | 
| GUIDED SHELL | 2007 | 
 | RU2351887C1 | 
| GUIDED MISSILE | 2008 | 
 | RU2370726C1 | 
| GUIDED MISSILE | 2002 | 
 | RU2222768C2 | 
| GUIDED MISSILE | 2008 | 
 | RU2370725C1 | 
| ROCKET | 2001 | 
 | RU2191983C1 | 
| GUIDED MISSLE | 2007 | 
 | RU2358229C2 | 
| METHOD OF GUIDED MISSLE LAUNCH | 2007 | 
 | RU2358232C2 | 
| GUIDED PROJECTILE | 2009 | 
 | RU2406063C1 | 
| GUIDED MISSILE | 2001 | 
 | RU2218546C2 | 
Authors
Dates
1997-07-20—Published
1994-09-12—Filed