FIELD: weapons and ammunition.
SUBSTANCE: set of invention relates to device for control over rocket or small-calibre jet projectiles. Proposed device comprises main lateral surface with nose level with one of its ends and means to initiate the powder. Device comprises combustion chamber filled with explosive powder. The latter comprises nanothermites. Jet projectile or rocket incorporates above describe control device.
EFFECT: perfected control.
11 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GLIDING AMMUNITION | 2012 |
|
RU2509287C1 |
| ROLLING CRUISE MISSILE | 2014 |
|
RU2544446C1 |
| METHOD FOR AUTOMATIC CONTROL OF HOMING HEAD, INSTALLED ON JET PROJECTILE, PARTICULARLY ON ROCKET | 2012 |
|
RU2595309C2 |
| HYPERSONIC ROCKET MISSILE | 2020 |
|
RU2754475C1 |
| FIREARMS AND SERVICE PROJECTILE FOR FIREARMS | 2009 |
|
RU2482421C2 |
| BOGDANOV'S METHOD OF SHAPED CHARGE DRILLING AND DEVICE FOR ITS REALISATION | 2012 |
|
RU2491402C1 |
| METHOD OF ANTITANK GUIDED MISSILE LAUNCH AND ANTITANK GUIDED MISSILE | 2006 |
|
RU2331041C1 |
| DEVICE CONTROLLING HIGH-MANEUVERABILITY ROCKET | 1998 |
|
RU2146353C1 |
| CARTRIDGE FOR SNIPER ARMS | 2014 |
|
RU2552406C1 |
| KINETIC ROCKET-AND-SPACE WEAPONRY SYSTEM | 2020 |
|
RU2752730C1 |
