|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
civil and military certification
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control system
|
|
gptkbp:cooling_system
|
air
air-cooled
|
|
gptkbp:customer_support
|
global support network
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:development
|
gptkb:M53_engine_family
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:elevation
|
up to 15,000 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
air start
upgradable for future needs
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
up to 5,000 hours
optimized for supersonic flight
|
|
gptkbp:engine_type
|
several variants available
|
|
gptkbp:first_flight
|
gptkb:1974
|
|
gptkbp:fuel_economy
|
high
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P45 engine
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:material
|
advanced alloys
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_history
|
used by several air forces
|
|
gptkbp:partnerships
|
collaborations with aerospace companies
|
|
gptkbp:propulsion
|
no
90 k N
75 k N/ton
|
|
gptkbp:related_aircraft
|
compatible with multiple aircraft types
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing R& D efforts
|
|
gptkbp:service_entry
|
gptkb:1979
|
|
gptkbp:successor
|
gptkb:RB199_engine
|
|
gptkbp:sustainability
|
designed for lower environmental impact
|
|
gptkbp:training
|
pilot and maintenance training available
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Panavia_Tornado
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:bfsLayer
|
6
|