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Hawker Siddeley P.1154
Planned British V/STOL fighter aircraft
Hawker Siddeley P.1154
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). Development originally started under P.1150, which was essentially a larger and faster version of the basic layout and technology being developed by the smaller subsonic Hawker Siddeley P.1127/Kestrel. A key difference of this design was the addition of plenum chamber burning, essentially an afterburner-like arrangement in the thrusters used during hover, greatly increasing their thrust. The release of NATO Basic Military Requirement 3 for a VTOL strike-fighter led to widespread industry participation. Hawker felt the P.1150 did not meet the requirements, so it was enlarged to become P.1150/3, and then renamed P.1154. This Mach 2-capable aircraft was the technical winner of the eleven submissions for NBMR-3, with the Dassault Mirage IIIV selected as a second design. Political infighting between the two groups and their various supporters...
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