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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:bore
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5.5 in
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gptkbp:compression_ratio
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5.5:1
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gptkbp:configuration
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V engine
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gptkbp:cooling_system
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liquid-cooled
water-cooled
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gptkbp:design
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gptkb:Rolls-Royce
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gptkbp:displacement
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27.0 L
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gptkbp:engine
|
historically significant
various aircraft models
advanced for its time
dual ignition system
influenced future designs
1915-1930s
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gptkbp:engine_configuration
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gptkb:V12
gptkb:V8_engine
detailed technical specifications available.
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gptkbp:engine_power
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high
excellent
1,800 rpm
149 k W
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gptkbp:engine_type
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reciprocating engine
multiple variants produced
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gptkbp:first_flight
|
1915
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gptkbp:fuel_capacity
|
136 kg
4 ft 6 in
2 ft 6 in
2 ft 0 in
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gptkbp:fuel_type
|
aviation gasoline
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Eagle
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gptkbp:ignition_system
|
spark ignition
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gptkbp:introduced
|
1915
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gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
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gptkbp:notable_users
|
gptkb:Royal_Air_Force
|
|
gptkbp:number_built
|
over 1,000
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gptkbp:power_output
|
200 hp
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gptkbp:propeller
|
variable pitch
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gptkbp:retired
|
1930s
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gptkbp:stroke
|
6.0 in
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gptkbp:successor
|
gptkb:Rolls-Royce_Kestrel
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gptkbp:torque
|
400 lb-ft
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gptkbp:type
|
gptkb:V8_engine
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gptkbp:used_in
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gptkb:aircraft
|
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gptkbp:valve_configuration
|
overhead valve
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gptkbp:weight
|
300 lb
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gptkbp:bfsParent
|
gptkb:Handley_Page_O/400
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gptkbp:bfsLayer
|
5
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