FIELD: aeronautical and space engineering; rocketry.
SUBSTANCE: proposed aircraft missile complex includes aircraft (8), launch vehicle (1), transportation and acceleration platform (5) with launch vehicle mounted on it by means of mechanical linkage and members, rope-lanyard (7) and systems ensuring proper functioning of missile complex. Mounted on launch vehicle body are wing with center-wing section (6), nose fairing (3) and tail fairing (4) with stabilizing surfaces mounted on it forming controllable stabilizer and vertical tail unit (10). Rope-lanyard is connected with center-wing section and with aircraft used as towing aircraft for towing the launch vehicle to point of launch.
EFFECT: enhanced efficiency of use of aircraft and missile complex as a whole.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIR ROCKET COMPLEX | 2009 |
|
RU2401777C1 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323855C2 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359870C2 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323856C2 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355602C2 |
| AVIATION ROCKET-LAUNCHING COMPLEX | 2005 |
|
RU2345927C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317921C1 |
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359881C2 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355601C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317920C1 |
