|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Rolls-Royce
|
|
gptkbp:development
|
gptkb:Rolls-Royce_RB.162
1950s to 1960s
|
|
gptkbp:emissions_standard
|
compliant with modern standards
|
|
gptkbp:engine
|
brayton cycle
|
|
gptkbp:engine_configuration
|
turbojet/turbofan hybrid
|
|
gptkbp:engine_type
|
gptkb:Pegasus_11-61
gptkb:Pegasus_11-61_R
gptkb:Pegasus_11-62
gptkb:Pegasus_11-63
gptkb:Pegasus_11-64
gptkb:Pegasus_11-65
gptkb:Pegasus_11-66
gptkb:Pegasus_11-67
gptkb:Pegasus_11-68
gptkb:Pegasus_11-69
gptkb:Pegasus_11-70
gptkb:Pegasus_11-71
gptkb:Pegasus_11-72
gptkb:Pegasus_11-73
gptkb:Pegasus_11-74
gptkb:Pegasus_11-75
gptkb:Pegasus_11-76
gptkb:Pegasus_11-77
gptkb:Pegasus_11-78
gptkb:Pegasus_11-79
gptkb:Pegasus_11-80
gptkb:Pegasus_11-81
gptkb:Pegasus_11-82
gptkb:Pegasus_11-83
gptkb:Pegasus_11-84
gptkb:Pegasus_11-85
gptkb:Pegasus_11-86
gptkb:Pegasus_11-87
gptkb:Pegasus_11-88
gptkb:Pegasus_11-89
gptkb:Pegasus_11-90
gptkb:Pegasus_11-91
gptkb:Pegasus_11-92
gptkb:Pegasus_11-93
gptkb:Pegasus_11-94
gptkb:Pegasus_11-95
gptkb:Pegasus_11-96
gptkb:Pegasus_11-97
gptkb:Pegasus_11-98
gptkb:Pegasus_11-99
|
|
gptkbp:exhaust_system
|
mixed flow exhaust
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
3.5 m
1.1 m
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Pegasus
|
|
gptkbp:inspired_by
|
gptkb:Rolls-Royce_RB.108
|
|
gptkbp:involved_technology
|
vectored thrust technology
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
vectoring thrust
|
|
gptkbp:notable_users
|
gptkb:US_Marine_Corps
|
|
gptkbp:number_of_stages
|
3 stages
|
|
gptkbp:operational_history
|
used by military aircraft
|
|
gptkbp:operational_use
|
gptkb:Royal_Air_Force
|
|
gptkbp:propulsion
|
22,000 lbf
14.7:1
|
|
gptkbp:related_aircraft
|
gptkb:Harrier_family
|
|
gptkbp:retirement
|
still in service
|
|
gptkbp:service_entry
|
gptkb:1969
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_F136
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:Harrier_Jump_Jet
|
|
gptkbp:bfsLayer
|
4
|