FIELD: flying vehicles. SUBSTANCE: method consists in including the load-bearing members into the flying vehicle structure which are removed in flight; load-bearing members are formed through local freezing of liquid substance effected during preflight preparation and/or during flight; working substance of flying vehicle, cryogenic fluid inclusive, may be used for the purpose. Liquid substance is frozen on structural member, for example on fuel tank by means of heat-exchange apparatus with cooled surfaces forming load-bearing member being frozen which is then thawed by heating the heat-exchange surfaces. EFFECT: enhanced efficiency. 8 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF EMERGENCY EMPTYING TANKS OF FLYING VEHICLES | 1992 |
|
RU2034752C1 |
| NON-EXPENDABLE SPACE TRANSPORTATION SYSTEM | 1992 |
|
RU2027638C1 |
| METHOD OF LAUNCHING NON-EXPENDABLE AEROSPACE SYSTEM | 1993 |
|
RU2046076C1 |
| TRANSPORT SPACE SYSTEM | 1992 |
|
RU2015079C1 |
| METHOD AND DEVICE FOR LAUNCHING FLYING VEHICLE | 1992 |
|
RU2005673C1 |
| METHOD OF INJECTION OF PAYLOAD INTO ORBIT | 1993 |
|
RU2092399C1 |
| METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY WITH LIQUID-PROPELLANT ENGINE PLANT | 1991 |
|
RU2046071C1 |
| AIRCRAFT ENGINE UNIT | 1995 |
|
RU2089743C1 |
| MULTISTAGE ROCKET | 1994 |
|
RU2088787C1 |
| CONTROLLABLE LIQUID-PROPELLANT MULTI-CHAMBER ROCKET VEHICLE | 1999 |
|
RU2156874C1 |
