Search results
Results from the WOW.Com Content Network
Gross weight: 16,100 kg (35,494 lb) combat weight Fuel capacity: approx 11,000 L (2,900 US gal; 2,400 imp gal) internal fuel Powerplant: 2 × SNECMA M53 afterburning turbofan engines, 64.3 kN (14,500 lbf) thrust each dry, 95.1 kN (21,400 lbf) with afterburner
Mirage F2: Strike fighter, a larger and more powerful version of the conventionally tailed F1. [4] Mirage G, G4 and G8: Variable-geometry (swing-wing) fighters. The G was effectively a swing-wing F2, while the G4 and G8 were twin-engined developments. [4] Mirage 4000 or Super Mirage 4000: Prototype larger version of the Mirage 2000 design.
The Mirage F1 emerged from a series of design studies performed by French aircraft manufacturer Dassault Aviation. [2] Having originally sought to develop a larger swept wing derivative of the Mirage III, which became the Mirage F2, to serve as a vertical take-off and landing propulsion testbed akin to the Dassault Mirage IIIV, however, it was soon recognized that the emerging design could ...
Flight testing started in July 1973 using a Caravelle flying test-bed and the engine first went supersonic in a Mirage F.1 test bed at the end of 1974. [ 3 ] The engine was designed to have better performance than the latest Atar engines but simpler and less costly than the SNECMA TF 306 turbofan. [ 1 ]
The Dassault Mirage IIIV, also spelled Mirage III V, was a French vertical take-off and landing prototype fighter aircraft of the mid-1960s developed and produced by Dassault Aviation. The Mirage IIIV was a VTOL derivative of an existing conventional fighter, the Dassault Mirage III ; the principal difference between the two types was the ...
The thrust-to-weight ratio is usually calculated from initial gross weight at sea level on earth [6] and is sometimes called thrust-to-Earth-weight ratio. [7] The thrust-to-Earth-weight ratio of a rocket or rocket-propelled vehicle is an indicator of its acceleration expressed in multiples of earth's gravitational acceleration, g 0. [5]
Dassault's resulting prototype, dubbed Mirage IV 01, looked a lot like the Mirage IIIA, even though it had double the wing surface, two engines instead of one, and twice the unladen weight. [3] The Mirage IV also carried three times more internal fuel than the Mirage III.
The Mirage 5 grew out of a request to Dassault from the Israeli Air Force.Since the weather over the Middle East is clear and sunny most of the time, the Israelis suggested removing the air intercept radar and its avionics, normally located behind the cockpit, from the standard Mirage IIIE to reduce cost and maintenance, and replacing them with more fuel storage for attack missions.