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gptkbp:instance_of
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gptkb:engine
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gptkbp:aircraft_operated
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compatible with multiple aircraft types
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gptkbp:application
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gptkb:aircraft
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gptkbp:average_temperature
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high
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gptkbp:certification
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civil and military certification
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gptkbp:check_in_time
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gptkb:battle
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gptkbp:controls
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gptkb:football_match
digital control system
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gptkbp:cooling_system
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air
air-cooled
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gptkbp:customer_support
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global support network
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gptkbp:developer
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gptkb:M53_engine_family
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gptkbp:diameter
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1.1 m
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gptkbp:elevation
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up to 15,000 m
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gptkbp:emissions_standard
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low
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gptkbp:engine
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twin-spool
air start
pylon-mounted
up to 5,000 hours
upgradable for future needs
optimized for supersonic flight
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gptkbp:engine_type
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axial compressor
high-pressure turbine
several variants available
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gptkbp:features
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modular design
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gptkbp:first_flight
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gptkb:1974
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gptkbp:fuel_capacity
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high
0.85 kg/k N/h
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gptkbp:fuel_type
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gptkb:Jet_A-1
annular combustor
dual fuel system
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|
https://www.w3.org/2000/01/rdf-schema#label
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M53-P45 engine
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gptkbp:is_tested_for
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extensively tested
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gptkbp:length
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4.5 m
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gptkbp:maintenance
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1,500 hours
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gptkbp:manufacturer
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gptkb:Rolls-Royce
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gptkbp:material
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advanced alloys
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gptkbp:max_speed
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Mach 2.2
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gptkbp:noise_level
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low
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gptkbp:operational_history
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used by several air forces
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gptkbp:partnerships
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collaborations with aerospace companies
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gptkbp:propulsion
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gptkb:battle
90 k N
75 k N/ton
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gptkbp:reliability
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high
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gptkbp:research_and_development
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ongoing R& D efforts
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gptkbp:services
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gptkb:1979
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gptkbp:successor
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R B199 engine
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gptkbp:sustainability
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designed for lower environmental impact
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gptkbp:training
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pilot and maintenance training available
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gptkbp:type
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gptkb:engine
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gptkbp:used_in
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gptkb:Panavia_Tornado
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gptkbp:weight
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1,200 kg
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gptkbp:bfsParent
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gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
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gptkbp:bfsLayer
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5
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