|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:controls
|
gptkb:football_match
digital control system
|
|
gptkbp:cooling_system
|
gptkb:currency
air-cooled
|
|
gptkbp:design
|
4,000 hours
|
|
gptkbp:developer
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
low
variable geometry
|
|
gptkbp:engine
|
modular design
mass production
twin-engine
developed in the 1970s
easy maintenance
air start
pylon-mounted
performance upgrades available
detailed specifications available.
R B199
optimized for supersonic flight
|
|
gptkbp:engine_type
|
axial compressor
high-pressure turbine
M53-P50 A
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1979
|
|
gptkbp:fuel_capacity
|
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-P50 engine
|
|
gptkbp:is_tested_for
|
ground testing
Rolls-Royce facility
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:propulsion
|
gptkb:battle
90 k N
110 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
gptkb:1982
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Panavia_Tornado
|
|
gptkbp:weight
|
1,500 kg
|