Rolls-Royce Tyne

URI: https://gptkb.org/entity/Rolls-Royce_Tyne

GPTKB entity

Predicate	Object
gptkbp:instanceOf	piston engine
gptkbp:application	gptkb:aircraft
gptkbp:compressionRatio	14-stage axial compressor
gptkbp:configuration	two-shaft
gptkbp:countryOfOrigin	gptkb:United_Kingdom
gptkbp:developedBy	gptkb:Rolls-Royce_Dart
gptkbp:diameter	0.76 m
gptkbp:enteredService	late 1950s
gptkbp:firstRun	1954
gptkbp:fuelType	aviation kerosene
gptkbp:hasTower	4-stage axial turbine
https://www.w3.org/2000/01/rdf-schema#label	Rolls-Royce Tyne
gptkbp:length	2.5 m
gptkbp:manufacturer	gptkb:Rolls-Royce
gptkbp:notableFor	high power output for its era
gptkbp:powerOutput	up to 6,100 shp
gptkbp:status	in service
gptkbp:type	turboprop
gptkbp:usedIn	gptkb:Transall_C-160 gptkb:Aeritalia_G.222_(early_prototypes) gptkb:Vickers_Vanguard gptkb:Short_Belfast gptkb:Breguet_Atlantique
gptkbp:weight	1,370 kg (approximate dry weight)
gptkbp:bfsParent	gptkb:Rolls-Royce_Dart gptkb:Bristol_Proteus gptkb:Canadair_CL-44 gptkb:Breguet_Atlantic_aircraft gptkb:Short_Belfast gptkb:Vickers_Vanguard_952 gptkb:Bristol_Proteus_engine gptkb:Rolls-Royce_Defence
gptkbp:bfsLayer	7