FIELD: designing of guided missiles and shot for artillery guns. SUBSTANCE: technique of launching of guided missile from artillery gun and shot includes guided missile 1 fastened in case 2 with propelling device 3, delayed-action pyrotechnic mechanism 4 and rocket engine 5; guided missile 1 is placed in artillery gun barrel 6 with breechblock 7. The missile tail bay accommodates magnetoelectric pulse generator 8, and safety device 9 is installed in alignment with it in the bottom of case 2, it is fastened to the case by means of pin 10. The windings of pulse generator 11 are connected via a wire coupling line to delayed-action pyrotechnic mechanism 12 of the functional units of the on-board systems and delayed- action pyrotechnic mechanism 4 of propelling device 3. Located in breechblock 7 is the firing mechanism, for instance firing pin 13. A pulse-shaping unit is provided in the shot, it includes pusher 14 rigidly coupled to generator 8, and safety device 9, a safety gap is formed between them. EFFECT: facilitated procedure. 2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF REMOVAL OF POWDER GASES FROM ARTILLERY GUN BARREL AND FIXED SHOT FOR ITS REALIZATION | 1994 |
|
RU2080540C1 |
SEPARATE LOADING SHOT | 1992 |
|
RU2072092C1 |
ARTILLERY GUIDE PROJECTILE | 1995 |
|
RU2096733C1 |
METHOD OF SHOOTING FROM CANNON UNITARY SHOT AND FIXED ROUND THEREFOR | 2015 |
|
RU2584405C1 |
ARTILLERY SHOT THROWER | 2014 |
|
RU2558533C1 |
METHOD AND DEVICE FOR TESTS OF MINE LAUNCHER SHOT | 2002 |
|
RU2228512C2 |
PROCESS INITIATING CONTROL SYSTEM OF ARTILLERY PROJECTILE, BALLISTIC CAP AND TIME FUSE OF GUIDED ARTILLERY PROJECTILE | 2000 |
|
RU2192615C2 |
FIXED ROUND | 1997 |
|
RU2114380C1 |
METHOD FOR REDUCING RECOIL FORCE OF FIREARMS AND GUN WITH FOLDING BARREL CHAMBER FOR IMPLEMENTATION THEREOF (EMBODIMENTS) | 2019 |
|
RU2736305C1 |
APPARATUS FOR TESTING CANNONS | 0 |
|
SU1733901A1 |
Authors
Dates
1997-05-27—Published
1995-03-07—Filed