FIELD: flying vehicles. SUBSTANCE: method consists in feeding the propellant through working passage of jet engine at definite relationship of consumption of oxidizer and fuel which differs from value at design flight mode. Relationship may increase and reduce in turn as compared with design flight mode. EFFECT: extended field of application of method. 2 cl
| Title | Year | Author | Number |
|---|---|---|---|
| NON-EXPENDABLE SPACE TRANSPORTATION SYSTEM | 1992 |
|
RU2027638C1 |
| METHOD OF TEMPORARY STRENGTHENING OF FLYING VEHICLE STRUCTURE AND FLYING VEHICLE MANUFACTURED BY THIS METHOD | 1992 |
|
RU2033947C1 |
| METHOD OF LAUNCHING NON-EXPENDABLE AEROSPACE SYSTEM | 1993 |
|
RU2046076C1 |
| METHOD AND DEVICE FOR LAUNCHING FLYING VEHICLE | 1992 |
|
RU2005673C1 |
| METHOD OF ALTITUDE THRUST CONTROL OF JET ENGINE | 1993 |
|
RU2076938C1 |
| METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY WITH LIQUID-PROPELLANT ENGINE PLANT | 1991 |
|
RU2046071C1 |
| METHOD OF INJECTION OF PAYLOAD INTO ORBIT | 1993 |
|
RU2092399C1 |
| MULTISTAGE ROCKET | 1994 |
|
RU2088787C1 |
| ENGINE FOR LIQUID-PROPELLANT ROCKET POWER PLANT | 1996 |
|
RU2119081C1 |
| CONTROLLABLE LIQUID-PROPELLANT MULTI-CHAMBER ROCKET VEHICLE | 1999 |
|
RU2156874C1 |
