Dassault Mirage IIIV ( Eng. Dassault Mirage IIIV , V - Russian. B, "vertical" ) - French experimental fighter-bomber vertical take-off and landing . Designed by the French company Dassault Aviation . One of the first VTOL aircraft to overcome the speed of sound .
| Mirage IIIV | |
|---|---|
 Mirage at the Paris Museum of Aviation and Cosmonautics | |
| Type of | GDP fighter bomber |
| Developer |  Dassault aviation |
| Manufacturer | |
| First flight | February 12, 1965 [1] |
| Status | the project was closed in 1968 [1] |
| Units produced | 3 (-1) |
| Base model | Dassault Mirage III |
Built two samples.
Content
History
The first flight is February 12, 1965 .
Flight performance
The calculated data for the serial machine are given.
Source [1]
Specifications
- Crew : 1 person
- Length : 18 m
- Wing span : 8.72 m
- Maximum take-off weight : 11,000 kg
- Engines:
- Marching engine Snecma TF-106
- engine type: two-circuit turbojet with afterburner
- quantity: 1
- Maximum traction : 1 Γ 7,600 kgf
- Rolls-Royce RB.162 lifting engine
- engine type: turbojet single-circuit
- quantity: 8
- Maximum traction : 8 Γ 1,600 kgf
- Marching engine Snecma TF-106
- Thrust for vertical take-off : 1.16
Flight performance
- Maximum speed :
- at design height: 2.3 M
- by the ground: 0.92 M
- Combat radius:
- at low altitude: 460 km
- at high altitude: 740 km
Armament
- Combat load: 900 kg
Notes
- β 1 2 3 Ruzhitsky E. I. European vertical take-off aircraft. - M .: Astrel , AST , 2000 .-- S. 234-239. - 256 s. - 10,000 copies. - ISBN 5-271-00863-0 (Astrel Publishing House LLC), ISBN 5-17-002848-2 (AST Publishing House LLC).