FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Transport aircraft for space rockets carrying and acceleration in stratosphere includes two fuselages, chassis, vertical stabilisers, engines, wing consisting of central part and two outer wing panels, where engines are mounted, and cradles-guides for attachment of the mentioned rockets. It is provided with additional wing with engines on consoles which are mounted on top ends of vertical stabilisers. Rear parts of fuselages are linked by aerodynamically clean crosspiece. The cradles-guides are attached to top surfaces of wing central part and on crosspiece.
EFFECT: increase in mass of space rockets brought into Earth stratosphere and improved controllability.
3 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF LAUNCHING SPACESHIPS BY REUSABLE SYSTEM AND SYSTEM FOR MULTIPLE LAUNCHING OF SPACESHIPS | 2010 |
|
RU2432303C1 |
| METHOD OF LAUNCHING SPACESHIPS BY REUSABLE SYSTEM AND SYSTEM FOR MULTIPLE LAUNCHING OF SPACESHIPS | 2010 |
|
RU2454355C1 |
| PASSENGERS AND CARGOES AIR TRANSPORTATION AND SYSTEM TO THIS END | 2012 |
|
RU2549728C2 |
| ROCKET-SPACE SYSTEM | 1993 |
|
RU2087389C1 |
| SUPER HEAVY-FREIGHT FLYING VEHICLE | 2006 |
|
RU2312042C2 |
| METHOD OF INJECTION OF OBJECTS INTO NEAR-EARTH ORBIT AND RECOVERABLE AERO-SPACE ROCKET AIRCRAFT-CARRIER FOR REALIZATION OF THIS METHOD (AERO-SPACE SYSTEM NUR-SAID SYSTEM) | 2001 |
|
RU2232700C2 |
| DEVICE FOR MASS DELIVERY OF TOURISTS TO STRATOSPHERE AND SUBSEQUENT RETURN TO GROUND | 2018 |
|
RU2730300C2 |
| COMPLEX SYSTEM FOR LAUNCHING HEAVY AEROSPACE SHUTTLES INTO ORBIT, SUPER-HEAVY JET AMPHIBIOUS AIRPLANE FOR SAID SYSTEM (VERSIONS) AND METHOD OF LAUNCHING | 2008 |
|
RU2397922C2 |
| METHOD OF SERVICING COSMIC ARTICLES AND SHUTTLE AEROSPACE SYSTEM FOR ITS IMPLEMENTATION | 2007 |
|
RU2342288C1 |
| AIRCRAFT FOR INTERCONTINENTAL FLIGHTS IN THE STRATOSPHERE | 2021 |
|
RU2758725C1 |
