FIELD: rocket technology.
SUBSTANCE: invention relates to multistage space rockets. Proposed rocket consists of an accelerating unit with liquid or solid-fuelled jet engines and a space module with a longitudinal channel having a toric shape with a cylindrical outer housing. Longitudinal channel is made in the form of a propulsive jet engine.
EFFECT: technical result is increased payload weight while the initial mass of the rocket does not change.
5 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT POWER UNIT | 2013 |
|
RU2601690C2 |
| METHOD OF HITTING ABOVE-WATER AND GROUND TARGETS WITH HYPERSONIC CRUISE MISSILE AND DEVICE THEREFOR | 2015 |
|
RU2579409C1 |
| METHOD OF PAYLOAD ORBITAL INJECTION BY REUSABLE SPACE TRANSPORT VEHICLE (VERSIONS) | 2006 |
|
RU2331551C2 |
| HELICOPTER OF COMBINED SCHEME | 2016 |
|
RU2641565C1 |
| VERTICAL TAKEOFF PROPELLER AIRCRAFT | 2015 |
|
RU2613074C2 |
| METHOD FOR TRANSFER OF WORKING FLUID FOR ENGINES OF SPACECRAFTS AND SYSTEM OF ITS IMPLEMENTATION | 2009 |
|
RU2385275C1 |
| ENGINE INSTALLATION FOR HYPERSONIC AND AIR SPACE FLYING VEHICLES | 1997 |
|
RU2133863C1 |
| SUBMARINE VESSEL | 2016 |
|
RU2623013C1 |
| ARMOUR-PIERCING SHELL | 2015 |
|
RU2588287C1 |
| METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD | 2012 |
|
RU2618831C2 |
