gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
|
gptkb:military_aircraft
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gptkbp:bore
|
5.5 in
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gptkbp:compression_ratio
|
5.5:1
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gptkbp:configuration
|
gptkb:V12
|
gptkbp:cooling_system
|
liquid cooling
water-cooled
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gptkbp:displacement
|
12.0 L
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gptkbp:engine
|
gptkb:Rolls-Royce_Limited
naturally aspirated
early 20th century technology
innovative for its era
influenced future aircraft engines
|
gptkbp:engine_configuration
|
V-type
classic design
front-mounted
RR200
|
gptkbp:engine_heritage
|
part of Rolls-Royce heritage
|
gptkbp:engine_legacy_influence
|
influenced later Rolls-Royce engines
|
gptkbp:engine_power
|
high reliability
good performance for its time
2000 rpm
149 k W
|
gptkbp:engine_service_life
|
1000 hours
|
gptkbp:engine_type
|
reciprocating engine
compatible with various aircraft models
multiple variants produced
|
gptkbp:exhaust_system
|
single exhaust
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gptkbp:fuel_capacity
|
3.5 ft
2.5 ft
2.0 ft
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce 200 HP
|
gptkbp:ignition_system
|
magneto
|
gptkbp:impact
|
significant impact on aviation history
|
gptkbp:maintenance
|
regular maintenance required
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
gptkbp:noise_level
|
low vibration
moderate noise
|
gptkbp:notable_users
|
gptkb:British_Royal_Air_Force
|
gptkbp:original_run
|
1915
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gptkbp:power_output
|
200 hp
|
gptkbp:production_years
|
1915-1920
|
gptkbp:stroke
|
6.0 in
|
gptkbp:successor
|
gptkb:Rolls-Royce_Eagle
|
gptkbp:torque
|
400 Nm
|
gptkbp:type
|
gptkb:V8_engine
|
gptkbp:used_in
|
gptkb:Royal_Aircraft_Factory_S._E.5
|
gptkbp:valve_timing
|
overhead valves
|
gptkbp:weight
|
200 kg
|
gptkbp:bfsParent
|
gptkb:Sir_Henry_Royce
|
gptkbp:bfsLayer
|
5
|