FIELD: rocketry.
SUBSTANCE: invention relates to the field of rocketry and can be used to create hypersonic cruise missiles designed to destroy ground and surface targets. The cruise missile contains a controllable warhead, which has a conical shape, and a sustainer stage, which includes an outer body, which is a cylindrical shell, on the outer surface of which a folding delta wing and tail unit are fixed, and an inner body consisting of a cylindrical shell, front and intermediate spherical heads, rear conical bottom, forming an oxidizer tank and a fuel tank, inside which a liquid-propellant rocket engine is installed. In this case, the outer and inner housings of the sustainer stage are installed coaxially and form an annular combustion chamber of a hypersonic ramjet engine, inside which a fuel manifold with nozzles and a flame stabilizer are installed.
EFFECT: objective of the invention is the possibility of using a rocket as an oxidizer of oxygen contained in the air in the atmospheric section of the flight path of a rocket.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CRUISE MISSILE | 2022 |
|
RU2790728C1 |
| REUSABLE CARRIER ROCKET STAGE | 2021 |
|
RU2766468C1 |
| ROCKET VEHICLE, RETURN STAGE OF ROCKET VEHICLE AND METHOD OF ITS LAUNCH UPON RETURN AND SYSTEM OF HELICOPTER PICK-UP OF RETURN STAGE | 2015 |
|
RU2609539C1 |
| AIR-DEFENSE MISSILE | 2008 |
|
RU2380650C1 |
| MULTISTAGED AIR-DEFENSE MISSILE | 2008 |
|
RU2380651C1 |
| METHOD OF HITTING ABOVE-WATER AND GROUND TARGETS WITH HYPERSONIC CRUISE MISSILE AND DEVICE THEREFOR | 2015 |
|
RU2579409C1 |
| MULTISTAGED CRUISE MISSILE | 2008 |
|
RU2380647C1 |
| LPE COMBUSTION CHAMBER MIXING HEAD | 2023 |
|
RU2815983C1 |
| RETURN CARRIER ROCKET STAGE | 2015 |
|
RU2603305C1 |
| RETURN STAGE OF ROCKET VEHICLE AND METHOD OF ITS OPERATION | 2015 |
|
RU2609547C1 |
