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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
Dassault Mirage 2000N/2000D; Dassault Mirage 4000; Dassault Mirage F1M-53; Specifications (M53-P2) Modules of M53 engine. ... Thrust-to-weight ratio: 6.5; See also
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]
Thrust/weight: 0.66 [158] Armament. Guns: 2× 30 mm (1.18 in) DEFA 553 cannons with 150 rounds per gun; Hardpoints: 1 centreline pylon, four underwing and two wingtip pylons with a capacity of 6,300 kg (13,900 lb) (practical maximum load 4,000 kg (8,800 lb)), with provisions to carry combinations of:
Dassault Mirage 4000: ... Indonesia postponed the acquisition of Mirage 2000 due to limited fiscal capacity. ... Thrust/weight: 0.7; Armament. Guns: ...
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.
Here’s a look back at their legendary residency at the Mirage through the decades. Siegfried and Roy pose with one of their tigers soon after they signed a five-year contract at the Mirage in 1987.
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio