FIELD: weapons and ammunition.
SUBSTANCE: missile includes case in the form of connected separable joint units with pyrotechnical burst connection of sealed head compartment with a sequence of homing head, inertial control system, ammunition, active thermal protection system and independent fluid or paste fuel propeller containing fuel with oxidiser and liquid-propellant rocket engine set with longitudinal nozzle, four liquid-propellant rocket engines with transverse nozzles and four liquid-propellant rocket engines generating head compartment torque, and propeller compartment with aerodynamic rudders, rudder drives, double-pulse solid fuel propeller aggregate, second pulse timing unit, correction unit.
EFFECT: efficient striking of high-altitude targets.
3 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
MISSILE | 2006 |
|
RU2327949C1 |
ANTI-AIRCRAFT GUIDED MISSILE 9M96 | 2020 |
|
RU2767645C1 |
METHOD FOR TARGET DESTRUCTION BY SPIN- STABILIZED BALLISTIC MISSILES | 1999 |
|
RU2158411C1 |
ROLL-STABILISED AIR BOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2006 |
|
RU2339904C2 |
ROLL-STABILISED AIR BOMB WITH INERTIAL-SATELLITE GUIDANCE SYSTEM | 2006 |
|
RU2339905C2 |
CRUISE MISSILE AND METHOD OF COMBAT USE THEREOF | 2017 |
|
RU2713546C2 |
INDIVIDUAL-USE GUIDED ANTI-AIRCRAFT MISSILE | 1996 |
|
RU2111445C1 |
ROCKET | 2005 |
|
RU2272984C1 |
AIRCRAFT GUIDED MISSILE | 2004 |
|
RU2259536C1 |
ROLLING CRUISE MISSILE | 2014 |
|
RU2544446C1 |
Authors
Dates
2015-04-20—Published
2014-05-15—Filed