FIELD: flying vehicles.
SUBSTANCE: proposed flying vehicle has fuselage for payload and ejection unit for acceleration of gas. Gas acceleration ejection unit includes at least two nozzles which are hermetically interconnected and at least one evacuated cavity which is communicated with reservoir. Two gas acceleration ejection units are mounted in succession. Nozzle of gas acceleration ejection unit is provided with cutoff device communicated with starting nozzle or with at least one navigation nozzle or with high-pressure receiver or with any combination of them. Cutoff device may be used for changing the area of gas flow including complete cutting-off of gas flow. Flying vehicle is also provided with at least two navigation nozzles which are hermetically interconnected.
EFFECT: extended field of application.
22 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2417926C2 |
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RU2338666C2 |
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RU2384471C2 |
| NOZZLE DEVICE | 2004 |
|
RU2303491C2 |
| NOZZLE ASSEMBLY | 2003 |
|
RU2267360C2 |
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|
RU2618183C2 |
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|
RU2279907C2 |
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|
RU2361679C2 |
| NOZZLE ASSEMBLY | 2003 |
|
RU2272678C2 |
| HEAD | 2005 |
|
RU2304471C1 |
