Rolls-Royce Spey 202

URI: https://gptkb.org/entity/Rolls-Royce_Spey_202
GPTKB entity
Statements (53)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Super_Étendard
gptkbp:application gptkb:aircraft
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter 3 ft 9 in
gptkbp:emissions_standard low
gptkbp:engine gptkb:Rolls-Royce_Spey_105
gptkb:Rolls-Royce_Spey_250
gptkb:Rolls-Royce_Spey_400
gptkb:Rolls-Royce_Spey_800
gptkb:Rolls-Royce_Spey_900
advanced aerodynamics
modular design
two
twin-spool
pylon-mounted
air-start
used in various military aircraft
influenced future engine designs.
used in various civilian aircraft
gptkbp:engine_type axial
afterburning turbofan
single-stage high-pressure, two-stage low-pressure
Spey 202, Spey 205, Spey 210
gptkbp:fan_engagement wide-chord
gptkbp:first_flight gptkb:1964
gptkbp:fuel_capacity high
gptkbp:fuel_type gptkb:Jet_A-1
annular
gptkbp:historical_site gptkb:Rolls-Royce_Spey_family
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce Spey 202
gptkbp:is_tested_for flight test
ground test
gptkbp:length 12 ft 6 in
gptkbp:maintenance 3,000 hours
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:max_speed Mach 2.2
gptkbp:noise_level low
gptkbp:operational_area gptkb:Lockheed_Martin_F-104_Starfighter
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
gptkb:Hawker_Siddeley_Buccaneer
BACTSR-2
gptkbp:operational_range 1,500 miles
gptkbp:propulsion 6.67
20,000 lbf
gptkbp:replaced_by gptkb:Rolls-Royce_RB.199
gptkbp:retirement_year 1990s
gptkbp:services gptkb:1965
gptkbp:successor gptkb:Rolls-Royce_RB.163
gptkbp:type gptkb:engine
gptkbp:weight 3,000 lb