FIELD: aviation.
SUBSTANCE: invention relates to aircraft and rocket equipment, to unmanned aerial vehicles and devices for their launching. Block of aircrafts with starting engine in transport-launching container is characterized by that starting engine is fixed to power farm. It is located in rear part of aircraft unit. They are fixed in the block by means of rods hinged to the power truss. On their inner surface there are attachment assemblies of aircrafts, and on their outer surface – slides. These sliders enter guides on transport-launching container and are fixed to them with pyro retainers. Aircraft block in the front part has an aircraft breeding assembly. It is connected with power frame. Transport launching container is detachable from carrier.
EFFECT: high reliability and efficiency of using aircraft assembly and reduced weight of the structure as a whole.
4 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REUSABLE MODULAR TRANSATMOSPHERIC VEHICLE | 2022 |
|
RU2787063C1 |
| AIRCRAFT (VERSIONS) | 2014 |
|
RU2547964C1 |
| METHOD OF AIRCRAFT START (VERSIONS) | 2014 |
|
RU2547963C1 |
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
| AEROSTAT ROCKET AND SPACE COMPLEX | 2019 |
|
RU2750558C2 |
| REUSABLE UNMANNED AERIAL VEHICLE IN A LAUNCHING CONTAINER AND A METHOD FOR LAUNCHING A REUSABLE UNMANNED AERIAL VEHICLE FROM A TRANSPORT LAUNCHING CONTAINER | 2019 |
|
RU2714616C1 |
| RECOVERABLE LAUNCH VEHICLE AND MULTIPLE CONFIGURRATION TRANSPORTATIOON SYSTEM | 1991 |
|
RU2035358C1 |
| AIRCRAFT TAKE-OFF ACCELERATOR | 2008 |
|
RU2373117C1 |
| SPACE ROCKET SYSTEM AND METHOD FOR RENDERING SERVICES IN LAUNCHING SPACE VEHICLES USING SPACE ROCKET SYSTEM | 2001 |
|
RU2179941C1 |
| METHOD FOR CONVERSION OF COMBAT SOLID-PROPELLANT ROCKETS INTO SOLID-PROPELLANT SPACE ROCKET AND SPACE ROCKET | 1998 |
|
RU2142898C1 |
