gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
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4
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gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_R-2800_Double_Wasp
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gptkbp:application
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gptkb:aircraft
|
gptkbp:compression_ratio
|
6.5:1
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gptkbp:controls
|
Manual Control
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gptkbp:cooling_system
|
Air-cooled
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gptkbp:displacement
|
2800 cubic inches
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gptkbp:emissions_standard
|
Single Exhaust
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gptkbp:engine
|
gptkb:Double_Wasp
gptkb:18
High Reliability
High Performance
Radial
2000 hp
1941-1960
2,700 RPM
Horizontally opposed
Fuselage Mount
Influenced Future Engine Designs
Single Intake
Widely Used in WWII
|
gptkbp:engine_type
|
Piston Engine
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gptkbp:first_flight
|
1941
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gptkbp:fuel_capacity
|
54 inches
40 inches
0.5 lb/hp/hr
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gptkbp:fuel_type
|
gptkb:Avgas
Carbureted
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-2800-10
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gptkbp:ignition_system
|
gptkb:Spark_Ignition
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gptkbp:maintenance
|
Routine Maintenance Required
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gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
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gptkbp:notable_users
|
gptkb:aircraft
gptkb:Philippine_Air_Force
gptkb:French_Air_Force
gptkb:military_base
gptkb:battle
|
gptkbp:power_output
|
2000 horsepower
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gptkbp:propulsion
|
Variable-pitch
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gptkbp:setting
|
Air-cooled
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gptkbp:successor
|
gptkb:R-4360_Wasp_Major
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gptkbp:torque
|
1,800 lb-ft
Wet Sump
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gptkbp:type
|
Radial Engine
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gptkbp:used_in
|
gptkb:aircraft
gptkb:Grumman_F8_F_Bearcat
gptkb:Douglas_DC-7
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gptkbp:weight
|
1,600 pounds
|