FIELD: rocket equipment.
SUBSTANCE: invention relates to a controlled reusable missile model, which comprises a cylindrical body including a main body part and an auxiliary body, with a head cowling mounted on the body apex; arranged inside housing engine and parachute system, wherein at the rocket body base the support-stabilizers with built-in range finder are installed; engine is an electric impeller installed inside lower part of housing, with air intake grid, wherein impeller is made with controlled nozzle; rocket main part comprises flight controller, onboard computer, accumulators and cable network; compensator motor with built-in impeller is built-in between main and auxiliary parts of rocket body.
EFFECT: technical result consists in improvement of safety and environmental friendliness.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTIFUNCTIONAL SMALL-SCALE TRANSFORMABLE REUSABLE UNMANNED AERIAL VEHICLE IN TRANSPORT-LAUNCH CONTAINER AND STARTING METHODS | 2022 |
|
RU2778177C1 |
| COASTAL AIR-ROCKET REUSABLE AUTONOMOUS COMPLEX | 2021 |
|
RU2768999C1 |
| "ПРПИ" LAUNCH VEHICLE VERTICAL TAKE-OFF AND LANDING SYSTEM | 2000 |
|
RU2187446C2 |
| ROCKET LAUNCH COMPLEX WITH A ROCKET-CATAPULT VEHICLE FOR FLIGHTS TO THE MOON AND BACK | 2020 |
|
RU2743061C1 |
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
| SYSTEM OF INJECTION OF PAYLOAD INTO LOW-ALTITUDE NEAR-EARTH ORBIT | 1997 |
|
RU2191145C2 |
| REUSABLE MISSILE AND AIRCRAFT UNIT AND WAY TO RETURN IT TO SPACEPORT | 2010 |
|
RU2442727C1 |
| PASSENGER AIRCRAFT WITH RESCUE MODULES AND COMBINED POWER PLANT | 2022 |
|
RU2781717C1 |
| SPACE ROCKET AND METHOD OF ITS LANDING (VERSIONS) | 2014 |
|
RU2568630C1 |
| MULTI-ELEMENT COMPOSITE AEROSPACE COMPLEX FOR VERTICAL TAKE-OFF AND LANDING IN THE SEA LAUNCH SYSTEM | 2021 |
|
RU2769791C1 |
