FIELD: transport.
SUBSTANCE: aviation rocket-launching complex includes airplane, carrier rocket of airborne launching, systems securing their functioning, transport-take-off platform and cable-halyard. Carrier rocket is equipped with wing, head and tail cowlings with stabiliser and vertical empennage installed. Wing variable sweep after take-off is foreseen. Cable-halyard is connected with wing centre-section and airplane is functioning as towplane for carrier rocket.
EFFECT: increase of admissible dimensions and launching mass of carrier rocket and spacecrafts launched to orbit.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323855C2 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355602C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317921C1 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323856C2 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359870C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317920C1 |
| AIR ROCKET COMPLEX | 2009 |
|
RU2401777C1 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355601C2 |
| AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2317923C2 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359881C2 |
