FIELD: military equipment.
SUBSTANCE: invention relates to the anti-aircraft and aviation air-to-air missiles. Anti-aircraft missile has two or more fuselages with jet engines. Between the fuselages there is a wing. On the wing sides the fuselages are made and placed so, that at supersonic speeds they act as the aerodynamic baffle plates. At that, the fuselages have approximately perpendicular to the wing tail fins. They enable the device stabilization in the transverse to the wing direction. There is a system with two wing surfaces, separated from the mid-wing by 120–150 degrees. One of them reduces the air overflow possibility from the increased pressure zone, and the second is the air suction into the rarefaction zone.
EFFECT: improvement in the missiles maneuverability.
1 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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|
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|
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|
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|
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|
RU2503592C1 |
| ATTACK AIRCRAFT (VERSIONS) | 2016 |
|
RU2623638C1 |
| SPACE ROCKET AND METHOD OF ITS LANDING (VERSIONS) | 2014 |
|
RU2568630C1 |
| PILOTLESS COMBAT AIRCRAFT /VERSIONS/ | 2016 |
|
RU2622327C1 |
