FIELD: armament.
SUBSTANCE: the rocket, made according to the canard aerodynamic configuration, has a cylindrical body, power unit with a fuel charge, engine thrust vector control unit, war equipment and control system equipment, four fixed wings with ailerons and their control mechanism. Installed in tandem with the wings are four aerodynamic control surfaces, four fixed destabilizers installed before the control surfaces and a device for determination of the rocket angles of attack. The device for determination of the rocket angles attack is provided with two devices for determination of the actual angles of attack, each including two airborne vane-type sensors lying in the same plane for determination of local angles of attack, former of the correcting signal, unit of corrections in Mach number function, g-sensor, filter, threshold device and a multiplexer.
EFFECT: enhanced rocket maneuverability.
2 cl, 13 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET | 1996 |
|
RU2094748C1 |
FLYING VEHICLE | 2005 |
|
RU2288435C1 |
AIRCRAFT GUIDED MISSILE | 2004 |
|
RU2259536C1 |
"CANARD" AERODYNAMIC CONFIGURATION ROCKET | 1997 |
|
RU2111446C1 |
MISSILE | 2019 |
|
RU2722329C1 |
ROLL-STABILISED AIR BOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2006 |
|
RU2339905C2 |
COUNTERAIR MISSILE | 2009 |
|
RU2439476C2 |
ROLL-STABILIZED HOMING AERIAL BOMB | 2003 |
|
RU2247314C1 |
ROCKET | 2004 |
|
RU2270413C1 |
ROLL-STABILISED AIR BOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2006 |
|
RU2339904C2 |
Authors
Dates
2006-03-27—Published
2005-04-19—Filed