FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed flight vehicle comprises payload compartment and ejection-type accelerator including nozzles, tightly intercommunicated, and vacuum chamber communicated with tank. Nozzle of said ejection-type accelerator is introduced inside said chamber to allow gas dynamic flow, coming out of the nozzle, to collide in said chamber.
EFFECT: power saving, higher maneuverability, expanded applications.
19 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHESTERENKO DEVICE FOR EJECTOR AIRCRAFT SPEED-UP | 2006 |
|
RU2338666C2 |
| SHESTERENKO'S AIRCRAFT (SAC) | 2006 |
|
RU2384471C2 |
| HEAT EXCHANGER HEATING METHOD OF THE HOUSES HEATING SYSTEM AND OTHER OBJECTS AND DEVICE FOR THE METHOD IMPLEMENTATION | 2012 |
|
RU2618183C2 |
| HEAD | 2005 |
|
RU2304471C1 |
| FLYING VEHICLE | 2003 |
|
RU2277059C2 |
| SHESTERENKO'S HEAD PIECE (VERSIONS) | 2006 |
|
RU2356637C2 |
| NOZZLE DEVICE | 2004 |
|
RU2303491C2 |
| NOZZLE HEAD | 2011 |
|
RU2551289C2 |
| NOZZLE ASSEMBLY | 2003 |
|
RU2272678C2 |
| SHESTERENKO SUPERNOZZLE (VERSIONS) | 2004 |
|
RU2361679C2 |
