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Dassault Mirage IIIV

Supersonic and Experimental Aircraft

The Dassault Mirage IIIV was a French vertical take-off and landing prototype fighter of the mid-1960s, built by Dassault Aviation as a VTOL derivative of the Dassault Mirage III. Its main difference from the Mirage III was a set of eight small vertical lift jets straddling the main engine, active only for take-off and landing. It was a response to the NATO Basic Military Requirement 3, which sought a supersonic-capable VTOL strike fighter, and it competed with the Hawker Siddeley P.1154. Two prototypes were built; the first began hovering trials on 12 February 1965, and the second reached Mach 2.04 in level flight in September 1966 before it was lost in an accident that November. The P.1154 won the requirement, the project was abandoned, and the surviving aircraft is on public display.

Facts
Year
1965 1
Engine Class
Jet 1
Engine Class
Turbofan 1
Status
Prototype 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Dassault Mirage IIIV (Wikipedia)

Of Make

Source Dassault Mirage IIIV (Wikipedia)
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Manufactured By

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Source Dassault Mirage IIIV (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
of the mid-1960s developed and produced by Dassault Aviation

Originated In

Also in Geography Atlas: where this subject originated.

Source Dassault Mirage IIIV (Wikipedia)Lead
Quote, Lead
is a French vertical take-off and landing (VTOL) prototype fighter aircraft
Sources
1. Dassault Mirage IIIV (Wikipedia)
  • Design and development
    conducted its first hovering trial on 12 February 1965
  • Specifications
    8 × Rolls-Royce RB162 turbojet engines
  • Specifications, engine class
    1 × Pratt & Whitney/SNECMA TF104 afterburning turbofan engine
  • Lead
    is a French vertical take-off and landing (VTOL) prototype fighter aircraft
  • Lead, manufacturer
    of the mid-1960s developed and produced by Dassault Aviation
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