FIELD: military equipment, applicable for production of warheads of high-precision small and medium-caliber guided missiles.
SUBSTANCE: the warhead has a fairing, explosive charge, fuse with a safety-actuating mechanism located in the cavity of the explosive charge bottom. The explosive charge is positioned between the fairing and the fuse, uniformly circumferentially positioned on the body side surface are proximity target sensors engageable with the safety-actuating mechanism, whose directional pattern is oriented perpendicularly to the warhead axis, and one or several sensing target sensors are installed on the end face surface of the fuse body, they are engageable with safety-actuating mechanism, whose directional pattern is oriented in the warhead axis.
EFFECT: enhanced efficiency of fragmentation at elementary objects located at the surface in the conditions of low angles of approach.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
TANDEM TYPE WARHEAD | 2003 |
|
RU2251069C1 |
HIGH-EXPLOSIVE NON-ISOTROPIC WARHEAD | 2006 |
|
RU2301958C1 |
HIGH-EXPLOSIVE WARHEAD | 2006 |
|
RU2301957C1 |
METHOD FOR WARHEAD ACTION MODE SWITCHING OF GUIDED MISSILE AND WARHEAD | 2005 |
|
RU2317513C2 |
HIGH-EXPLOSIVE WARHEAD | 2004 |
|
RU2269739C1 |
MISSILE MUNITION | 2020 |
|
RU2769035C1 |
METHOD FOR DETERMINATION OF PROXIMITY FUSE RANGE IN FLIGHT TESTS OF GUIDED MISSILE | 2003 |
|
RU2231017C1 |
METHOD FOR DETERMINATION OF PROXIMITY FUSE-RANGE AT TESTS OF GUIDED MISSILE | 2005 |
|
RU2294526C1 |
GUIDED MISSILE | 2004 |
|
RU2278351C1 |
SHELL | 2001 |
|
RU2194941C1 |
Authors
Dates
2005-03-10—Published
2003-06-23—Filed