Hawker Siddeley P.1154

Length
14.9352 m
Flat Wing Span
7.3152 m
Max Mach
1.3 Mach
Max Ceiling
14935.2 m
Number of Engines
1
Maximum Take-Off Weight
14.0478 t (paragliders: kg)

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
Hawker Siddeley P.1154 14.0478

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All data (17 fields)
Name
Hawker Siddeley P.1154
Manufacturer
Hawker Siddeley
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).
Designer
Hawker Siddeley
Type
V/STOL combat aircraft
Length (m)
14.9352
Cockpit Crew
1
Max Ceiling (m)
14935.2
Armament
4
Max Mach (Mach)
1.3
National Origin
United Kingdom
Powerplant Description
1 × Bristol Siddeley BS.100/9 Plenum-chamber burning vectored thrust turbofan engine
Primary Users
Royal Air Force (intended), Royal Navy (intended)
Status
Cancelled, 1965
Wikipedia Article (URL)
en.wikipedia.org/wiki/Hawker_Siddeley_P.1154
Flat Wing Span (m)
7.3152
Number of Engines
1