Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aircraft
|
| gptkbp:built |
post-World_War_II
|
| gptkbp:community |
part of aviation history
|
| gptkbp:controls |
hydraulic control
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
3 ft 6 in
|
| gptkbp:displacement |
significant in military aviation
|
| gptkbp:engine |
compact design
pylon-mounted influenced future designs subject of research studies extensive technical documentation available early jet technology pioneered turbojet technology recognized in aviation heritage. used in engineering education used in various test aircraft |
| gptkbp:engineConfiguration |
turbojet
developed in 1940s |
| gptkbp:engineType |
axial compressor
single-stage turbine starter motor compatible with various airframes multiple variants developed |
| gptkbp:exhibits |
displayed in aviation museums
|
| gptkbp:firstRace |
1948
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuelType |
kerosene
axial flow |
| https://www.w3.org/2000/01/rdf-schema#label |
Armstrong Siddeley Lynx
|
| gptkbp:is_used_in |
gptkb:Hawker_Siddeley_Harrier
|
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Armstrong_Siddeley
|
| gptkbp:noise_level |
85 dB
|
| gptkbp:notable_feature |
Lynx Mk. 1
|
| gptkbp:operational_status |
1950s
|
| gptkbp:origin |
gptkb:United_Kingdom
|
| gptkbp:performances |
high reliability
high thrust-to-weight ratio moderate complexity |
| gptkbp:propulsion |
2.5:1
3,000 lbf |
| gptkbp:related_engine |
gptkb:Rolls-Royce_Avon
influenced jet engine design |
| gptkbp:retirementYear |
1970s
|
| gptkbp:successor |
gptkb:Rolls-Royce_RB.162
|
| gptkbp:team_achievements |
first operational turbojet in UK
|
| gptkbp:type |
turbojet engine
|
| gptkbp:weight |
1,200 lb
|