FIELD: aviation.
SUBSTANCE: invention relates in particular to designs of unmanned aerial systems. The unmanned aerial missile system contains a reusable aviation returnable missile (RATM) with a high-precision guided munition having a frontal guidance kit and a range extension kit installed behind it. The missile has a modular design that can be used with various types of bombs and their guidance units, and with the possibility of automatic vertical landing on the tail of the RATM by means of a propeller-jet system. The propeller-jet system includes a turbojet engine with a controlled thrust vector and power take-off for the drive of coaxial two-bladed main rotors (TMR), which enables flight at altitude with the X-shaped front fins, rear wing and pulling TMR or with folded TMR blades, respectively, to attack the target or for a mortar launch from a vertical transport and launch container.
EFFECT: increased flight range, reduced dimensions in the transport position, possibility of repeated use.
2 cl, 1 tbl, 3 ex
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UNMANNED AIRCRAFT SYSTEM | 2023 |
|
RU2823932C1 |
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|
RU2768999C1 |
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RU2769000C1 |
COMBAT AIRCRAFT COMPLEX WITH UNMANNED AERIAL VEHICLE | 2023 |
|
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ATTACK WEAPON AVIATION COMPLEX | 2021 |
|
RU2778159C1 |
AIR MISSILE SYSTEM WITH AN UNMANNED PERCUSSIVE AIRCRAFT HELICOPTER | 2018 |
|
RU2710317C1 |
UNOBTRUSIVE AIRCRAFT-MISSILE SYSTEM | 2019 |
|
RU2725372C1 |
STEALTHY ROCKET AND AIRCRAFT COMPLEX | 2019 |
|
RU2722609C1 |
UNMANNED IMPACT HELICOPTER AIRCRAFT | 2019 |
|
RU2733678C1 |
Authors
Dates
2023-03-13—Published
2022-05-04—Filed