FIELD: armament.
SUBSTANCE: the guided missile has a detachable zero stage, sustainer stage with nose cone, nose air intake, body with air-dynamic control actuator and aerodynamic controls. The sustainer stage of the missile uses a heat-exchange device, whose input is connected to the input of the air intake, and the output - to the input of the gas distributing device of the control actuator.
EFFECT: enhanced reliability of the guided missile.
5 dwg, 1 ex
| Title | Year | Author | Number |
|---|---|---|---|
| HYPERSONIC GUIDED MISSILE | 2005 |
|
RU2308670C1 |
| METHOD OF FIRING ANTIAIRCRAFT GUIDED ROCKET AND ROCKET FOR ITS REALIZATION | 2001 |
|
RU2191985C2 |
| METHOD FOR CHECKING OF FUNCTIONING OF AIR-DYNAMIC CONTROL ACTUATOR OF GUIDED MISSILES OR ROCKETS AND DEVICE FOR ITS REALIZATION | 2001 |
|
RU2218548C2 |
| GUIDED ANTI-AIRCRAFT MISSILE | 2000 |
|
RU2167390C1 |
| ROLLING CRUISE MISSILE | 2014 |
|
RU2544446C1 |
| DEVICE FOR ACCELERATED DELIVERY OF PASSENGERS TO INTERCONTINENTAL DISTANCES | 2019 |
|
RU2731518C1 |
| METHOD OF INJECTION OF OBJECTS INTO NEAR-EARTH ORBIT AND RECOVERABLE AERO-SPACE ROCKET AIRCRAFT-CARRIER FOR REALIZATION OF THIS METHOD (AERO-SPACE SYSTEM NUR-SAID SYSTEM) | 2001 |
|
RU2232700C2 |
| RADIO-CONTROLLED ANTI-AIRCRAFT MISSILE | 2000 |
|
RU2189003C2 |
| TWO-STAGE GUIDED MISSILE | 2007 |
|
RU2357201C2 |
| CONTROLLED BULLET | 2012 |
|
RU2512047C1 |
