About: Hawker Siddeley P.1154

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

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). Developed alongside the subsonic and smaller Hawker Siddeley P.1127/Kestrel, the P.1154 was derived from the P.1150. The P.1150 proposal did not meet NATO Basic Military Requirement 3 and, consequently, the P.1154 was born. This Mach 2-capable platform retained plenum chamber burning previously designed for the P.1150. Although the technical winner out of eleven submissions, follow-on testing and production for the P.1154 did not proceed as a result of political strife.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Hawker Siddeley P.1154
rdfs:comment	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). Developed alongside the subsonic and smaller Hawker Siddeley P.1127/Kestrel, the P.1154 was derived from the P.1150. The P.1150 proposal did not meet NATO Basic Military Requirement 3 and, consequently, the P.1154 was born. This Mach 2-capable platform retained plenum chamber burning previously designed for the P.1150. Although the technical winner out of eleven submissions, follow-on testing and production for the P.1154 did not proceed as a result of political strife.
sameAs	dbr:Hawker_Siddeley_P.1154
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max takeoff weight alt	14050.0
length alt	15.07 m
span main	731.52
Status	Cancelled, 1965
thrust alt	147 kN
primary user	Royal Air Force
Type	V/STOL combat aircraft
length main	1506.22
span alt	7.32 m
Manufacturer	Hawker Siddeley
max speed main	Mach 1.3 at sea level
ceiling main	49000.0
National Origin	United Kingdom
type of jet	vectored-thrust turbofan engine with PCB
Developed From	Hawker Siddeley P.1127
thrust original
more users	Royal Navy
engine (jet)	Bristol Siddeley BS.100/9
max speed alt	Mach 2.0 at altitude
jet or prop?	jet
thrust main	33000(xsd:integer)
number of jets	1(xsd:integer)
plane or copter?	plane
ceiling alt	15,000 m
max takeoff weight main	30970.0
Crew	1(xsd:integer)
Armament	*2 x 1000 lb bombs
Designer	dbkwik:resource/EH7bR4KwNm0IGPButVv0zw==
ref	The British Fighter since 1912
abstract	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). Developed alongside the subsonic and smaller Hawker Siddeley P.1127/Kestrel, the P.1154 was derived from the P.1150. The P.1150 proposal did not meet NATO Basic Military Requirement 3 and, consequently, the P.1154 was born. This Mach 2-capable platform retained plenum chamber burning previously designed for the P.1150. Although the technical winner out of eleven submissions, follow-on testing and production for the P.1154 did not proceed as a result of political strife. Meanwhile, HSA considered modifying the airframe for a joint specification for an aircraft by the RAF and Royal Navy. Between 1961 and 1965 the two services harmonised their specifications to preserve design commonality. However, the RAF's desired configuration was to take precedence over that of the Royal Navy's. A number of proposals were submitted – at one stage, a twin-Spey design was considered, then rejected. Following the Labour government's coming to power in 1965, the project was cancelled. The Royal Navy would acquire the F-4 Phantom, while the RAF continued to foster development of the P.1127 (RAF), leading to the successful Harrier family.
is Developed Into of	Hawker Siddeley P.1127
is major applications of	Bristol Siddeley BS100

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