FIELD: armament.
SUBSTANCE: the high-explosive non-isotropic warhead has a burster and a blasting device, which includes safety-actuating mechanisms, whose terminal assemblies are radially shifted relative to the burster axis, contact target sensor, radiometric noncontact target sensor for fixing the target and determining the side of flight at large misses, optical noncontact target-sensor designed for determining the side of flight at small misses, as well as an electronic unit for computation of the blast delay time, provided with a device for generation of a command for actuation of the safety-actuating mechanism, whose terminal assembly is shifted to the side opposite the flight side.
EFFECT: enhanced efficiency of warhead action.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
HIGH-EXPLOSIVE WARHEAD | 2006 |
|
RU2301957C1 |
MISSILE MUNITION | 2020 |
|
RU2769035C1 |
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END | 2009 |
|
RU2398182C1 |
TANDEM TYPE WARHEAD | 2003 |
|
RU2251069C1 |
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END | 2009 |
|
RU2398183C1 |
METHOD FOR WARHEAD ACTION MODE SWITCHING OF GUIDED MISSILE AND WARHEAD | 2005 |
|
RU2317513C2 |
HIGH-EXPLOSIVE WARHEAD | 2003 |
|
RU2247928C1 |
METHOD TO CONTROL CHARACTERISTICS OF EFFECTIVE FIELD OF HIGH-EXPLOSIVE WARHEAD OF MISSILE AND DEVICE FOR ITS REALISATION | 2011 |
|
RU2484419C1 |
INDIVIDUAL-USE GUIDED ANTI-AIRCRAFT MISSILE | 1996 |
|
RU2111445C1 |
HIGH-EXPLOSIVE WARHEAD | 2004 |
|
RU2269739C1 |
Authors
Dates
2007-06-27—Published
2006-01-10—Filed