FIELD: technical devices for equipment of ammunition warheads with an on-board power source, mainly of guided rockets or missiles having of cruise engine.
SUBSTANCE: the safety-actuating mechanism is characterized by the fact that it has a double-acting electrical detonator for equipment of the main detonator of the ammunition warhead, firing arming system, standard fitting system, self-destruction system and a system of protection at non-standard situations. The self-destruction system has an inertia starting mechanism, electric igniter, pyrotechnical self-destruction track, primer cap and a burned-through gasket, and the system of protection at non-standard situations has a shutter, contact coupled to it, shunting double-acting electrical detonator and an inertia mechanism.
EFFECT: enhanced reliability and safety of operation of the ammunition in standard and non-standard conditions.
3 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SAFETY AND ARMING UNIT OF GUIDED MUNITIONS | 2006 |
|
RU2333458C9 |
| SAFE-AND-ACTUATE MECHANISM OF MISSILE WARHEAD | 2007 |
|
RU2380653C2 |
| SAFETY AND ARMING UNIT | 2017 |
|
RU2671017C1 |
| NOSE PERCUSSION FUSE | 2002 |
|
RU2211437C1 |
| SAFETY-LAUNCHING DEVICE OF THE ON-BOARD EARTH-BASED AUTOMATION DETONATION CIRCUIT | 2015 |
|
RU2625660C2 |
| NOSE FUZE | 2006 |
|
RU2341765C2 |
| SMALL-SIZED IMPACT FUSE | 2003 |
|
RU2242704C1 |
| GRENADE LAUNCHER ROUND | 2006 |
|
RU2341763C2 |
| BASE FUZE | 1997 |
|
RU2125706C1 |
| NOSE FUSE | 2005 |
|
RU2307310C1 |
