FIELD: rocket technics.
SUBSTANCE: invention relates to rocket engineering. In the method for controlling the target's defeat by a cruise missile (CM) after CM launching and flying along individual trajectory, selecting the target and approaching the target, removing the stages of protecting the combat equipment at a given distance to the target, determined from the conditions of the imminent defeat of the target, a data array is formed according to a given algorithm in the CM onboard equipment. Array contains the CM number, the type of the warhead, the target number in the target order and the target coordinates, the distance to the target at the time the data array is completed. It is possible to transfer the generated data array to the CM carrier. In addition, it may be possible to transmit a data set before the command to blast the warhead with a predetermined time interval, including at least one repeater.
EFFECT: ensuring the autonomy and speed of delivery of information about the defeat of the target.
11 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TARGET HITTING BY SUPERSONIC CRUISE MISSILE AND DEVICE TO THIS END | 2014 |
|
RU2569971C1 |
| METHOD OF HITTING VULNERABLE GROUND TARGETS BY SUPERSONIC MISSILE AND DEVICE TO THIS EFFECT | 2008 |
|
RU2377493C2 |
| TARGET DESTRUCTION METHOD BY VOLLEY OF ATMOSPHERIC AIRCRAFTS | 2016 |
|
RU2691233C2 |
| ANTISUBMARINE CRUISE MISSILE AND ITS APPLICATION METHOD | 2014 |
|
RU2546726C1 |
| METHOD OF HITTING A REMOTE GROUP PROTECTED TARGET | 2018 |
|
RU2730792C2 |
| METHOD FOR TARGET DAMAGE BY SUPERSONIC CRUISE MISSILE AND SUPERSONIC CRUISE MISSILE FOR ITS IMPLEMENTATION | 2016 |
|
RU2644962C2 |
| FLIGHT METHOD OF ROLLING MISSILE | 2014 |
|
RU2544447C1 |
| METHOD OF CRUISE MISSILE HOMING | 2019 |
|
RU2723783C1 |
| CRUISE MISSILE WITH SELF-CONTAINED UNMANNED UNDERWATER VEHICLE-MINE | 2018 |
|
RU2714274C2 |
| ADAPTIVE AIRBORNE MISSILE SYSTEM | 2019 |
|
RU2720592C1 |
