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