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Hawker Siddeley P.1154 ✕ Dassault Mirage 5 ✕
Manufacturer Hawker Siddeley Dassault Aviation
Description The Hawker Siddeley P.1154 was a planned supersonic vertical/short take-off and landing (V/STOL) fighter aircraft designed by Hawker Siddeley Aviation (HSA). The Dassault Mirage 5 is a French supersonic attack aircraft/fighter-bomber designed by Dassault Aviation during the 1960s and manufactured in France and other countries.
ICAO Code MIRA
First Flight 1967-05-19
Designer Hawker Siddeley Dassault Aviation
Type V/STOL combat aircraft Attack aircraft , Fighter-bomber
Length (m) 14.9352 15.55
Height (m) 4.5
Cockpit Crew 1 1
Max Speed (km/h) 2350
Cruise Speed (km/h) 956
Max Ceiling (m) 14935.2 18000
Armament 4 2 × 30 mm (1.18 in) DEFA 552 cannons with 125 rounds per gun; 4,000 kg (8,800 lb) of payload on five external hardpoints, including a variety of bombs, reconnaissance pods or Drop tanks; 2 × Matra JL-100 drop tank/rocket pack, each with 18 × SNEB 68 mm rockets and 66 US gallons (250 liters) of fuel; 2 × AIM-9 Sidewinder OR Matra R550 Magic
Max Mach (Mach) 1.3
National Origin United Kingdom France
Number Built 582
Powerplant Description 1 × Bristol Siddeley BS.100/9 Plenum-chamber burning vectored thrust turbofan engine 1 × SNECMA Atar 9C afterburning turbojet, 41.97 kN thrust each
Primary Users Royal Air Force (intended), Royal Navy (intended) French Air Force (historical), Belgian Air Force (historical) , Egyptian Air Force (historical) , Pakistan Air Force
Status Cancelled, 1965 Active
Wikipedia Article (URL) en.wikipedia.org/wiki/Hawker_Siddeley_P.1154 en.wikipedia.org/wiki/Dassault_Mirage_5
Flat Wing Span (m) 7.3152 8.22
Flat Wing Area (m²) 35
Wake Category M
Number of Engines 1 1