Properties (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:component |
sensors
compressor exhaust system turbine combustor nozzle fuel pump control system air intake heat exchanger accessory gearbox thrust reverser starter motor engine monitoring system fuel control unit oil system vibration damper engine_mount |
| gptkbp:compressionRatio |
6:1
|
| gptkbp:controls |
hydraulic system
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
Axial-flow
|
| gptkbp:developer |
Orenda_14_series
|
| gptkbp:diameter |
3 ft 6 in
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:engineConfiguration |
single-spool
|
| gptkbp:exhaustSystem |
afterburning
|
| gptkbp:facilities |
Orenda_test_center
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuel_capacity |
0.8 lb/lbf/hr
|
| gptkbp:fuelType |
Jet A
spark plug |
| https://www.w3.org/2000/01/rdf-schema#label |
Orenda 14V
|
| gptkbp:inventor |
Orenda_14_prototype
|
| gptkbp:is_used_in |
Canadair CL-13 Sabre
|
| gptkbp:legacy |
Canadian_aviation_history
|
| gptkbp:length |
14 ft 6 in
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
Orenda_Engines
|
| gptkbp:market |
military aviation
|
| gptkbp:maximum_speed |
Mach_0.9
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:number_of_stages |
8
|
| gptkbp:operationalHistory |
gptkb:Royal_Canadian_Air_Force
|
| gptkbp:patentCitation |
engine technology
|
| gptkbp:performance |
high thrust-to-weight ratio
|
| gptkbp:propulsion |
14,000 lbf
|
| gptkbp:related_engine |
gptkb:Rolls-Royce_Avon
|
| gptkbp:retirementYear |
1970s
|
| gptkbp:service_ceiling |
45,000 ft
|
| gptkbp:successor |
Orenda_15
|
| gptkbp:team |
Orenda_engineers
|
| gptkbp:type |
turbojet engine
|
| gptkbp:weight |
1,800 lb
|