FIELD: weapons and ammunition.
SUBSTANCE: invention relates to weapons and can be used in small-size rocket systems. Controlled bullet comprises armor-piercing rod, stabilizing elements, aerodynamic rudders, control unit drive unit, photodetector, onboard hardware and on-board power supply. Bullet is equipped with series-connected voltage stabilizer connected to the on-board power supply source, and a constant voltage amplifier. Said amplifier provides a supply voltage value of the modulating pulse generator at a level of not lower than 80 V. There is a modulating pulse generator which generates control signals modulated by a high-frequency rectangular signal with frequency of not less than 10 kHz ± 10 %, in accordance with onboard hardware control commands. Drive unit of control elements is made piezoelectric in the form of two piezoelectric elements and lever rigidly connected with axis of aerodynamic steering wheels.
EFFECT: technical result is improved maneuvering properties of controlled bullet and increased accuracy of firing.
1 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
CONTROLLED BULLET | 2019 |
|
RU2713831C1 |
GUIDED BULLET | 2013 |
|
RU2538881C1 |
METHOD OF INCREASING ACCURACY OF RIFLED ARMS AND DEVICE OF ITS IMPLEMENTATION | 2015 |
|
RU2603334C2 |
CONTROLLED BULLET | 2012 |
|
RU2496089C1 |
BULLET CONTROL METHOD AND CONTROLLED BULLET | 2019 |
|
RU2719802C1 |
ROLL-STABILISED AIR BOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2006 |
|
RU2339905C2 |
METHOD AND DEVICE FOR INITIATING AN AIR-DYNAMIC STEERING DRIVE OF A GUIDED AERIAL BOMB, A METHOD FOR CHECKING THE READINESS OF AN AIR-DYNAMIC STEERING DRIVE BEFORE DROPPING A GUIDED AERIAL BOMB, AN AIR-DYNAMIC STEERING GEAR AND CONTROL EQUIPMENT FOR AN AIR-DYNAMIC STEERING DRIVE OF AN AERIAL BOMB | 2020 |
|
RU2748828C1 |
GUIDED JET PROJECTILE | 2012 |
|
RU2502042C1 |
GUIDED MISSILE IN TRANSPORTER-LAUNCHER CONTAINER | 2012 |
|
RU2518126C2 |
HIGH-ACCURACY BANK-STABILISED DAY-HIGHT ALL-WEATHER AVIABOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2007 |
|
RU2346232C1 |
Authors
Dates
2019-12-11—Published
2019-02-14—Filed