|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:airlines
|
30 kg/s
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
FADEC
digital control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
200 kg
air-cooled
air start
pylon mounted
|
|
gptkbp:engineConfiguration
|
turbojet
single_spool
|
|
gptkbp:engineType
|
axial
afterburning turbofan
single_spool
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
100 liters
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark plug
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 30000
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:launchDate
|
30 seconds
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maxSpeed
|
1,200 km/h
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:numberOfEpisodes
|
1
|
|
gptkbp:operationalStatus
|
1500 K
|
|
gptkbp:propulsion
|
no
20:1
jet propulsion
3000 lbf
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:relatedTo
|
gptkb:Adour_Mk_951
|
|
gptkbp:retired
|
in service
|
|
gptkbp:services
|
15,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedBy
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:South_African_Air_Force
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
150 kg
|