|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Bell_206_L-4
|
|
gptkbp:application
|
gptkb:Mc_Donnell_Douglas_MD_500
gptkb:Bell_206
gptkb:Agusta_A109
helicopters
Eurocopter A S350
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:average_temperature
|
up to 700 ° C
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
10:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
direct air cooling
|
|
gptkbp:design
|
modular design
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
axial exhaust
|
|
gptkbp:engine
|
electric starter
free turbine
flexible mount
|
|
gptkbp:engine_type
|
gptkb:engine
centrifugal compressor
single-stage turbine
C20 R
C20 A
C20 B
C20 D
C20 E
C20 F
C20 M
C20 S
C20 W
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce 250-C20 R
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
gptkb:aircraft
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:power_output
|
420 shp
|
|
gptkbp:powers
|
3.5 k W/kg
|
|
gptkbp:propulsion
|
420 lbf
|
|
gptkbp:services
|
3000 hours
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:weight
|
120 kg
|