FIELD: weapons.
SUBSTANCE: kinetic warhead with aerodynamic guidance comprises a sharpened nose part and a tail part connected to the nose part by means of a bearing. On the nose part there are fixed helical aerodynamic elements, which serve for its untwisting when entering the atmosphere. Tail part contains aerodynamic control surfaces, bearing wing fixed in the warhead centre of mass location zone, braking aerodynamic element performing the function of orientation of the entire device at the initial stage of entry into the atmosphere and retracted during flight through the atmosphere.
EFFECT: high accuracy of targeting high-manoeuvrable, high-speed and small targets.
10 cl, 13 dwg
Title | Year | Author | Number |
---|---|---|---|
KINETIC ROCKET-AND-SPACE WEAPONRY SYSTEM | 2020 |
|
RU2752730C1 |
INTERCEPTOR MISSILE | 2021 |
|
RU2814225C2 |
METHOD OF GUIDING ANTI-MISSILE TO SUPERSONIC TARGET | 2022 |
|
RU2825905C2 |
HYPERSONIC ROCKET MISSILE | 2020 |
|
RU2754475C1 |
ROCKET CONTROL SYSTEM WITH MULTISTAGE SOLID FUEL ENGINE | 2021 |
|
RU2804562C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2742496C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2021 |
|
RU2805888C2 |
ANTI-MISSILE GUIDANCE METHOD | 2021 |
|
RU2814291C2 |
MISSILE AND METHOD FOR ITS OPERATING | 2014 |
|
RU2590760C2 |
SPACECRAFT TO DE-ORBIT SATELLITE AND DE-ORBITING METHOD | 2005 |
|
RU2334656C2 |
Authors
Dates
2024-08-19—Published
2022-05-30—Filed