FIELD: aeronautical and space engineering. SUBSTANCE: gas dynamic pulse of thrust is created in direction opposite to acceleration of vehicle which is achieved by interaction of reaction jet of cruise engine of flying vehicle with flow deflector located on launching trolley. EFFECT: reduced mass of launching trolley in case of emergency braking. 3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY PROVIDED WITH ELECTROMAGNETIC DRIVE | 1991 |
|
RU2046070C1 |
| METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY WITH LIQUID-PROPELLANT ENGINE PLANT | 1991 |
|
RU2046071C1 |
| NON-EXPENDABLE SPACE TRANSPORTATION SYSTEM | 1992 |
|
RU2027638C1 |
| METHOD OF LAUNCHING NON-EXPENDABLE AEROSPACE SYSTEM | 1993 |
|
RU2046076C1 |
| METHOD OF INJECTION OF PAYLOAD INTO ORBIT | 1993 |
|
RU2092399C1 |
| METHOD OF EMERGENCY EMPTYING TANKS OF FLYING VEHICLES | 1992 |
|
RU2034752C1 |
| MOBILE LAUNCHER UNIT | 2020 |
|
RU2739477C1 |
| METHOD OF ALTITUDE CONTROL OF OVEREXTENDED REACTION NOZZLE FOR ROCKET ENGINE | 1999 |
|
RU2164618C1 |
| METHOD OF FORMING THE SYSTEM OF FORCES OF FLYING VEHICLE AND FLYING VEHICLE-GROUND-AIR-AMPHIBIAN FOR REALIZATION OF THIS METHOD | 2006 |
|
RU2317220C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
