FIELD: rocket equipment.
SUBSTANCE: invention relates to the field of military equipment, namely to munition of surface-to-surface, surface-to-air, and air-to-air missiles, and can be used in the development of guided missiles, anti-ballistic missiles, and ballistic missiles. The high-explosive warhead of a directional missile comprises an electronic unit for calculating the detonation time delay, contact and non-contact target sensors, a bursting charge, and safety and arming mechanisms installed thereon, wherein the detonators of said mechanisms are radially displaced relative to the axis of the charge. A three-coordinate all-angle multi-lobe optical or radio location near-location station is applied as a non-contact target position sensor. The detonators of the safety and arming mechanisms are connected into a multipoint initiation system configured to initiate all detonators of the safety and arming mechanisms according to a time cyclogram calculated by the electronic unit for calculating the detonation time delay.
EFFECT: increase in the density of the field of striking elements and the launching velocity thereof in the direction of the target.
1 cl, 3 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| INDIVIDUAL-USE GUIDED ANTI-AIRCRAFT MISSILE | 1996 | 
 | RU2111445C1 | 
| METHOD FOR WARHEAD ACTION MODE SWITCHING OF GUIDED MISSILE AND WARHEAD | 2005 | 
 | RU2317513C2 | 
| HIGH-EXPLOSIVE NON-ISOTROPIC WARHEAD | 2006 | 
 | RU2301958C1 | 
| HIGH-EXPLOSIVE WARHEAD | 2006 | 
 | RU2301957C1 | 
| HIGH-EXPLOSIVE WARHEAD | 2004 | 
 | RU2269739C1 | 
| TANDEM TYPE WARHEAD | 2003 | 
 | RU2251069C1 | 
| GUIDED ANTI-AIRCRAFT MISSILE | 2002 | 
 | RU2222770C1 | 
| COMBAT SECTION OF GUIDED MISSILE | 2002 | 
 | RU2247927C2 | 
| HIGH-EXPLOSIVE WARHEAD | 2003 | 
 | RU2247928C1 | 
| METHOD AND DEVICE (AMMUNITION) FOR DESTRUCTION OF GROUND AND AIR TARGETS | 1999 | 
 | RU2158408C1 | 
Authors
Dates
2022-03-28—Published
2020-11-19—Filed