M53-P40 engine

GPTKB entity

Statements (55)
Predicate Object
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 gptkb:electronic
electronic control unit (ECU)
gptkbp:cooling_system liquid cooling
water-cooled
radiator and fan
gptkbp:displacement 30.6 L
gptkbp:emissions_standard Euro III
gptkbp:engine gptkb:V12
V-type
armored vehicles
cast iron
high reliability
single turbocharger
high torque at low RPM
variable geometry
flat torque curve
rubber mounts
exhaust manifold and silencer
gptkbp:engine_type gptkb:standard
M53-P40 A, M53-P40 B
gptkbp:first_introduced gptkb:1980s
gptkbp:fuel_capacity 50 L
200 L/100 km
length 1,200 mm
width 800 mm
height 800 mm
gptkbp:fuel_type diesel
common rail
fuel tank and lines
https://www.w3.org/2000/01/rdf-schema#label M53-P40 engine
gptkbp:ignition_system diesel ignition
gptkbp:is_tested_for MTU test facility
gptkbp:launch_site electric starter
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:MTU_Friedrichshafen
gptkbp:max_speed 2,600 RPM
800-2,600 RPM
gptkbp:noise_level 85 d B
gptkbp:power_output 1500 hp
gptkbp:propulsion 1.25 hp/kg
gptkbp:services over 10,000 hours
gptkbp:successor M93 engine
gptkbp:torque wet sump
5000 Nm
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:Leopard_2_tank
gptkbp:valve_configuration DOHC
gptkbp:weight 1,200 kg