|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:breathability
|
turbocharged
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
electronic control unit (ECU)
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
12.7 L
|
|
gptkbp:durability
|
long-lasting
|
|
gptkbp:emissions_standard
|
Euro III
after-treatment system
|
|
gptkbp:engine
|
various applications
aluminum alloy
high performance
cast iron
modern design
V engine
high reliability
advanced features
single turbocharger
detailed specifications available
high output
V12 configuration
idle at 800 rpm
900 k W
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:first_introduced
|
gptkb:1994
|
|
gptkbp:frequency
|
500 hours
|
|
gptkbp:fuel_capacity
|
40 L
200 L/100 km
|
|
gptkbp:fuel_type
|
diesel
diesel fuel
common rail
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P34 engine
|
|
gptkbp:is_tested_for
|
extensively tested
|
|
gptkbp:launch_site
|
electric starter
|
|
gptkbp:maintenance
|
scheduled maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:max_speed
|
2,500 rpm
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:power_output
|
1200 hp
|
|
gptkbp:setting
|
gptkb:V12
|
|
gptkbp:successor
|
gptkb:M53-P40_engine
|
|
gptkbp:torque
|
wet sump
4,500 Nm
6,000 Nm
|
|
gptkbp:type
|
turbocharged diesel engine
|
|
gptkbp:used_in
|
gptkb:Challenger_2_tank
|
|
gptkbp:valve_configuration
|
DOHC
|
|
gptkbp:weight
|
1,200 kg
|