FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used in development of carrier rockets. Carrier rocket comprises shuttle booster with jet stabilisation system connected to second stage and reusable elements. Said reusable booster consists of rocket unit with liquid-propellant rocket engines connected with aircraft complex composed of airframe with variable-sweep wings and aerodynamic controls, horizontal stabiliser, undercarriage, air breathers with their fuel tanks and nose compartment. Nose compartment fitted at rocket unit has pilot cabin and controlled swing baffles the number of which corresponds to that of joint points between nose compartment and second stage. Recesses are made at said joints. Air breathers are secured at variable-sweep wing surfaces and furnished with controlled protective shields. Stabiliser is composed of two fins arranged at wings. Even number of throttled air breathers are arranged in reusable rocket booster in symmetry about crosswise axis, parallel with wings, along its lengthwise axis.
EFFECT: increased payload, higher reliability, reparability and portability.
4 cl, 12 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
| REUSABLE MISSILE AND AIRCRAFT UNIT AND WAY TO RETURN IT TO SPACEPORT | 2010 |
|
RU2442727C1 |
| MULTI-ELEMENT COMPOSITE AEROSPACE COMPLEX FOR VERTICAL TAKE-OFF AND LANDING IN THE SEA LAUNCH SYSTEM | 2021 |
|
RU2769791C1 |
| ACCELERATING CARRIER AIRCRAFT (VERSIONS) | 2019 |
|
RU2715816C1 |
| GLIDING SPACESHIP (VERSIONS) WITH FOLDING NOSE CONE AND METHOD OF CONTROLLING ITS DESCENT TO AIRFIELD | 2011 |
|
RU2479469C1 |
| RETURN STAGE OF ROCKET VEHICLE, METHOD OF ITS OPERATION AND GAS TURBINE ENGINE | 2015 |
|
RU2609664C1 |
| RETURN STAGE OF ROCKET VEHICLE AND METHOD OF ITS OPERATION | 2015 |
|
RU2609549C1 |
| RETURN STAGE OF ROCKET VEHICLE AND METHOD OF ITS OPERATION | 2015 |
|
RU2609547C1 |
| RETURN CARRIER ROCKET STAGE | 2015 |
|
RU2603305C1 |
| CARRIER ROCKET FIRST STAGE FLY-BACK BOOSTER BUILT AROUND UNIFIED ROCKET UNIT | 2012 |
|
RU2492123C1 |
