|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
vertical takeoff and landing
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
gptkb:Pegasus_210
gptkb:Pegasus_380
gptkb:Pegasus_320
gptkb:Pegasus_330
high bypass ratio
axial compressor
Pegasus 105
Pegasus 110
Pegasus 115
Pegasus 120
Pegasus 130
Pegasus 150
Pegasus 160
Pegasus 170
Pegasus 180
Pegasus 190
Pegasus 200
Pegasus 220
Pegasus 230
Pegasus 240
Pegasus 250
Pegasus 260
Pegasus 270
Pegasus 280
Pegasus 290
Pegasus 300
Pegasus 310
Pegasus 340
Pegasus 350
Pegasus 360
Pegasus 370
Pegasus 390
Pegasus 400
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:historicalEvent
|
1960s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Pegasus
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Holdings
|
|
gptkbp:maximum_speed
|
gptkb:Mach_1.0
|
|
gptkbp:notable_feature
|
vectored thrust
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Navy
gptkb:United_States_Marine_Corps
gptkb:Spanish_Air_Force
|
|
gptkbp:operationalHistory
|
1970s to present
|
|
gptkbp:propulsion
|
22,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Rolls-Royce_RB
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_F136
|
|
gptkbp:technology
|
VTOL
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
1,500 lb
|