|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
1,500 °C
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:engine
|
1,000 mm
1,200 lb
1,800 mm
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
turbofan
axial
single stage high pressure
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:firstRace
|
1964
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark plug
hydromechanical
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 242
|
|
gptkbp:inspiration
|
training and light attack
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
gptkb:Adour_Mk_871
|
|
gptkbp:operational_status
|
1970s
|
|
gptkbp:origin
|
gptkb:United_Kingdom
|
|
gptkbp:propulsion
|
2.92
3,500 lbf
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_871
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
1,200 lb
|