FIELD: aviation.
SUBSTANCE: invention is related to the field of aviation rocket-space engineering. Aviation rocket complex comprises airplane, carrier rocket for air starting, the following components installed on it - wing, front and tail fairings, on tail fairing stabilising surfaces are installed, which create controlled stabiliser and for instance vertical tail empennage. Also aviation rocket complex comprises towing rope-halyard that is connected to wing center section and airplane that performs functions of carrier rocket towing device, transport-overspeed platform with carrier rocket installed on it and systems that provide for their functioning. Transport-overspeed platform represents an airplane that has residual resource and service life and is redesigned for installation and surface transportation of carrier rocket.
EFFECT: invention is aimed at increase of carrier rocket dimensions and starting weight and therefore weights of spacecrafts put in orbit are reduced.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AVIATION ROCKET COMPLEX | 2005 |
|
RU2359870C2 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323856C2 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355601C2 |
| AVIATION ROCKET-LAUNCHING COMPLEX | 2005 |
|
RU2345927C2 |
| AIR ROCKET COMPLEX | 2009 |
|
RU2401777C1 |
| AIRCRAFT MISSILE SYSTEM | 2006 |
|
RU2323855C2 |
| AIRCRAFT MISSILE COMPLEX | 2005 |
|
RU2317923C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317921C1 |
| AEROSPACE ROCKET COMPLEX | 2006 |
|
RU2355602C2 |
| AIRCRAFT MISSILE COMPLEX | 2006 |
|
RU2317920C1 |
