gptkbp:instance_of
|
gptkb:engine
|
gptkbp:bfsLayer
|
5
|
gptkbp:bfsParent
|
gptkb:MD_530_G_Cayuse_Warrior
gptkb:OH-58_D
|
gptkbp:application
|
helicopters
|
gptkbp:armament
|
gptkb:3
|
gptkbp:average_temperature
|
-40 to 50 ° C
|
gptkbp:compression_ratio
|
16:1
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:diameter
|
0.4 m
|
gptkbp:drivetrain
|
reduction gearbox
|
gptkbp:emissions_standard
|
single exhaust
ICAO Chapter 4
|
gptkbp:engine
|
gptkb:Rolls-Royce_250
30 seconds
3000 hours
|
gptkbp:engine_type
|
gptkb:engine
C20 R
C30 A
C30 B
C30 D
C30 E
C30 F
C30 G
C30 M
C30 P
C30 S
|
gptkbp:first_flight
|
gptkb:1960
|
gptkbp:fuel_capacity
|
120 kg
1.2 m
0.4 m
0.5 kg/hp/hr
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce 250-C30 R
|
gptkbp:launched
|
starter-generator
|
gptkbp:length
|
1.2 m
|
gptkbp:maintenance
|
500 hours
|
gptkbp:manufacturer
|
gptkb:film_production_company
|
gptkbp:max_speed
|
42000
|
gptkbp:notable_users
|
gptkb:Agusta_Westland
gptkb:Bell_Helicopter
gptkb:Eurocopter
gptkb:Mc_Donnell_Douglas
|
gptkbp:power_output
|
450 shp
|
gptkbp:powers
|
3.75 k W/kg
|
gptkbp:propulsion
|
3.75
3.75 hp/kg
|
gptkbp:service_ceiling
|
20,000 ft
|
gptkbp:setting
|
turbo-shaft
|
gptkbp:weight
|
120 kg
|