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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustor_type
|
axial flow
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:design_date
|
gptkb:World_War_II
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
modular design
post-war development
early turbojet technology
influential in jet engine design
|
|
gptkbp:engine_configuration
|
turbojet
RR.100
Rolls-Royce design
|
|
gptkbp:engine_power
|
high performance
high reliability
1,000 hours
good efficiency
|
|
gptkbp:engine_tested
|
ground testing
|
|
gptkbp:engine_thrust
|
3,500 lbf
|
|
gptkbp:engine_type
|
gptkb:Derwent_I
gptkb:Derwent_II
multiple airframes
|
|
gptkbp:first_flight
|
gptkb:1944
|
|
gptkbp:fuel_capacity
|
1,200 lb
12 ft 6 in
3 ft 4 in
|
|
gptkbp:fuel_type
|
gptkb:gasoline
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Derwent XXV
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
moderate noise
|
|
gptkbp:number_of_stages
|
two
|
|
gptkbp:operational_use
|
jet propulsion
|
|
gptkbp:power_output
|
3,500 lbf
|
|
gptkbp:propulsion
|
0.29
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Derwent_V
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:de_Havilland_Vampire
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Derwent
|
|
gptkbp:bfsLayer
|
6
|