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
Engine Class Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Dassault Mirage IIIV (Wikipedia)
Of Make
Source Dassault Mirage IIIV (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Dassault Mirage IIIV (Wikipedia)Lead, manufacturerQuote, 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)LeadQuote, 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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