Adour Mk 951-16

GPTKB entity

Statements (42)
Predicate Object
gptkbp:instanceOf jet engine
gptkbp:aircraft trainer aircraft
gptkbp:application military training
light attack aircraft
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:coolingSystem air-cooled
gptkbp:design Rolls-Royce_design_team
gptkbp:developer gptkb:Adour_engine_family
gptkbp:diameter approximately 2.5 ft
gptkbp:emissionsStandard low emissions
gptkbp:engineType axial compressor
single-stage turbine
gptkbp:fanBase single-stage fan
gptkbp:fuel_capacity high fuel efficiency
0.8 lb/hp/hr
gptkbp:fuelType gptkb:Jet_A-1
spark ignition
annular combustor
https://www.w3.org/2000/01/rdf-schema#label Adour Mk 951-16
gptkbp:introduced 1980s
gptkbp:is_used_in gptkb:BAE_Systems_Hawk
gptkbp:length approximately 3.5 ft
gptkbp:maintenance 1,000 hours
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:noise_level low noise
gptkbp:notableUsers gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Saudi_Arabian_Air_Force
gptkbp:operational_status pilot training
combat training
aerobatic training
gptkbp:operationalHistory in service since 1980s
gptkbp:operationalRange up to 30,000 ft
gptkbp:performance high thrust-to-weight ratio
gptkbp:propulsion approximately 4,000 lbf
gptkbp:related_engine gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
gptkbp:successor gptkb:Adour_Mk_951
gptkbp:type turbofan engine
gptkbp:weight approximately 1,200 lb