FIELD: weapons and ammunition.
SUBSTANCE: guided missile comprises fair, tandem combat part comprising leading shaped charge (LSC) and main combat part, and extending head part. Fair has bottom with LSC seat. LSC casing is arranged in nose fair to form a closed chamber between nose fair and LSC casing front end face that communicates, via a channel, with pulsed pressure source. Extending front part represents a set of hollow telescopic links and compression spring. Extreme inner link has a nose shell with orifice and electric contact element. Extreme outer link has a dead bottom and is arranged to axially move in guide sleeve fastened on nose fair. The latter accommodates locking element representing a plug with normalised break-off force. Guide sleeve and telescopic mechanism outer link have outer link locking element.
EFFECT: higher efficiency.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED SHELL | 2007 |
|
RU2351887C1 |
GUIDED MISSILE | 2008 |
|
RU2370726C1 |
GUIDED MISSILE | 2007 |
|
RU2351886C1 |
GUIDED MISSILE | 2001 |
|
RU2218546C2 |
METHOD OF GUIDED MISSLE LAUNCH | 2007 |
|
RU2358232C2 |
CONTACT DEVICE | 2008 |
|
RU2380654C1 |
GUIDED MISSILE | 1994 |
|
RU2084809C1 |
GUIDED PROJECTILE | 2009 |
|
RU2406063C1 |
GUIDED MISSLE | 2007 |
|
RU2358229C2 |
CONTACT DEVICE | 2001 |
|
RU2206061C2 |
Authors
Dates
2009-10-20—Published
2008-07-09—Filed