enow.com Web Search

Search results

  1. Results from the WOW.Com Content Network
  2. Dassault Mirage 4000 - Wikipedia

    en.wikipedia.org/wiki/Dassault_Mirage_4000

    The Mirage 4000 was noticeably larger and heavier than the single-engined Mirage 2000, the 4000 having two SNECMA M53-2 turbofans. [1] It also featured small canards above the engine air intakes and a true bubble canopy, compared to the Mirage 2000 and previous Mirages.

  3. Snecma M53 - Wikipedia

    en.wikipedia.org/wiki/SNECMA_M53

    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 ]

  4. Dassault Mirage - Wikipedia

    en.wikipedia.org/wiki/Dassault_Mirage

    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.

  5. Thrust-to-weight ratio - Wikipedia

    en.wikipedia.org/wiki/Thrust-to-weight_ratio

    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]

  6. Template:Engine thrust to weight table - Wikipedia

    en.wikipedia.org/wiki/Template:Engine_thrust_to...

    Template: Engine thrust to weight table. 1 language. ... Merlin 1D rocket engine, full-thrust version 467 1,030 825 185,000 180.1 References

  7. Dassault Mirage F1 - Wikipedia

    en.wikipedia.org/wiki/Dassault_Mirage_F1

    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 ...

  8. Dassault Mirage IIIV - Wikipedia

    en.wikipedia.org/wiki/Dassault_Mirage_IIIV

    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 ...

  9. Dassault Mirage IV - Wikipedia

    en.wikipedia.org/wiki/Dassault_Mirage_IV

    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.