FIELD: military.
SUBSTANCE: two-system guided missile in a transport and launch container contains an on-board connector, a detachable starting engine, a warhead, a propulsion system with booster and sustainer engines, a propulsion engine launch unit, a gyroscopic roll sensor, an angular velocity sensor, a photoreceiving device, an on-board radio equipment unit, and an on-board power supply, digital processing unit, decoder, microcontroller, data bus and steering compartment connected in a certain way.
EFFECT: ensures an increase in the controlled flight range and a reduction in the near firing zone.
1 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE IN TRANSPORTER-LAUNCHER CONTAINER | 2012 |
|
RU2518126C2 |
| GUIDED MISSILE | 2005 |
|
RU2292009C1 |
| GUIDED MISSILE | 2005 |
|
RU2272240C1 |
| MULTIMISSION GUIDED MISSILE IN LAUNCHING PACK | 2004 |
|
RU2277693C1 |
| METHOD OF FIRING ANTIAIRCRAFT GUIDED ROCKET AND ROCKET FOR ITS REALIZATION | 2001 |
|
RU2191985C2 |
| ANTIAIRCRAFT SELF-CONTAINED COMPLEX OF SUBMARINE SELF-DEFENSE (SDS "SPIDER") AND METHOD OF ITS USE | 2008 |
|
RU2382313C2 |
| GUIDED MISSILE | 2005 |
|
RU2288437C1 |
| GUIDED MISSILE | 2022 |
|
RU2772089C1 |
| BULLET CONTROL METHOD AND CONTROLLED BULLET | 2019 |
|
RU2719802C1 |
| CONTROLLED BULLET | 2019 |
|
RU2713831C1 |
