FIELD: ammunition, in particular, combat sections of "air-to-air", "ground-to-air" guided missiles.
SUBSTANCE: the combat section of the guided missile is provided with four transceiving units and five AND gates located in a laser proximity fuse, the output of each transceiving unit is connected to one input of two respective AND gates, connected to whose second input is the output of the adjacent transceiving unit. The output of each AND gate is connected to the inputs of the signal processing unit, whose respective outputs via a safety-actuating mechanism are connected to six respective electric detonators of the initiating device located in six hitting members having shaped explosive charges with metal facings with a large corner radius on the end faces. Six hitting members and six receivers of reflected signals of the respective transceiving units re located symmetrically and uniformly in the parallel planes of the cross section in diameter with the longitudinal axes of symmetry perpendicular to the missile longitudinal axis in such a way that the plane formed by the longitudinal axis of the hitting member and the missile longitudinal axis is positioned at a similar distance from the two receivers of reflected signals adjacent to it. The invention provides for hitting of armored and usually air targets at misses up to 50 to 100 m due to a high kinetic energy of the "shaped nucleus" formed at blasting, oriented in the direction of the target of the hitting member.
EFFECT: enhanced probability of target hitting.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
COMBINATION BURSTING CHARGE | 2002 |
|
RU2239774C2 |
MULTIMISSION GUIDED MISSILE IN LAUNCHING PACK | 2004 |
|
RU2277693C1 |
DETONATOR | 2007 |
|
RU2362969C2 |
METHOD FOR WARHEAD ACTION MODE SWITCHING OF GUIDED MISSILE AND WARHEAD | 2005 |
|
RU2317513C2 |
TWO-STAGE ANTITANK GUIDED MISSILE | 2012 |
|
RU2527610C2 |
MULTIMODE FUSE | 2024 |
|
RU2824453C1 |
METHOD TO CONTROL CHARACTERISTICS OF EFFECTIVE FIELD OF HIGH-EXPLOSIVE WARHEAD OF MISSILE AND DEVICE FOR ITS REALISATION | 2011 |
|
RU2484419C1 |
GUIDED MISSILE IN TRANSPORTER-LAUNCHER CONTAINER | 2012 |
|
RU2518126C2 |
ROLL-STABILIZED AERIAL BOMB WITH LASER HOMING HEAD | 2005 |
|
RU2300075C1 |
AC ACTIVE PROTECTION METHOD AND SYSTEM FOR ITS IMPLEMENTATION (VERSIONS) | 2015 |
|
RU2601241C2 |
Authors
Dates
2005-03-10—Published
2002-07-29—Filed