Rolls-Royce R V12 B

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:aircraft
gptkbp:compression_ratio 6.5:1
gptkbp:controls mechanical
gptkbp:cooling_system liquid-cooled
water-cooled
gptkbp:displacement 27 liters
gptkbp:engine gptkb:battle
gptkb:Rolls-Royce_V12_series
high reliability
high power-to-weight ratio
longitudinal
influential in aviation history
R-1
V-type engine
inline engine design
detailed specifications available
used in various aircraft models
excellent performance
limited production run
3,000 RPM
various modifications made
historically significant engine
V12 engine configuration
1,200 k W
gptkbp:engine_type reciprocating engine
multiple variants produced
gptkbp:first_introduced gptkb:World_War_II
gptkbp:fuel_capacity 800 mm
1,200 mm
600 mm
550 kg
gptkbp:fuel_type aviation gasoline
carbureted
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce R V12 B
gptkbp:ignition_system dual ignition
gptkbp:is_tested_for extensively tested
gptkbp:manufacturer gptkb:Rolls-Royce_Limited
gptkbp:notable_users gptkb:Hawker_Hurricane
gptkb:noble_title
gptkb:starship
gptkbp:power_output 1,600 hp
gptkbp:production_years 1940s
gptkbp:setting gptkb:V12
gptkbp:successor gptkb:Rolls-Royce_R_V12_C
gptkbp:torque 1,500 Nm
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:aircraft
gptkbp:valve_configuration overhead valve
gptkbp:weight approximately 1,200 lbs
gptkbp:bfsParent gptkb:Rolls-Royce_R_V12
gptkbp:bfsLayer 4