|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:bore
|
5.5 in
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:cylinderCount
|
5 cylinders
|
|
gptkbp:displacement
|
5.0 L
|
|
gptkbp:engineConfiguration
|
horizontally opposed
|
|
gptkbp:firstFlight
|
1925
|
|
gptkbp:fuelType
|
aviation gasoline
magneto
|
|
gptkbp:historical_significance
|
used in early military aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright J-5 engine
|
|
gptkbp:is_used_in
|
gptkb:Wright_Model_T
gptkb:Wright_Model_M
gptkb:Wright_Model_Q
gptkb:Wright_Model_W
gptkb:Wright_Model_G
gptkb:Wright_Model_R
gptkb:Boeing_Model_40
gptkb:Wright_Model_S
gptkb:Wright_Model_N
gptkb:Wright_Model_B
gptkb:Wright_Model_Z
gptkb:Wright_Model_E
gptkb:Wright_Model_H
gptkb:Wright_Model_O
gptkb:Wright_Model_Y
gptkb:Wright_Model_I
gptkb:Wright_Model_C
gptkb:Curtiss_JN-4
gptkb:Wright_Model_K
gptkb:Wright_Model_J
gptkb:Wright_Model_P
gptkb:Wright_Model_L
gptkb:Wright_Model_D
gptkb:Wright_Flyer
gptkb:Wright_Model_V
gptkb:Wright_Model_F
gptkb:Wright_Model_U
gptkb:Wright_Model_X
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notableUsers
|
gptkb:United_States_Navy
gptkb:United_States_Army_Air_Service
|
|
gptkbp:performance
|
good performance for its time
|
|
gptkbp:powerOutput
|
200 hp
|
|
gptkbp:produces
|
over 10,000 units
|
|
gptkbp:productionYears
|
1925-1935
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:stroke
|
5.5 in
|
|
gptkbp:successor
|
Wright_J-6_engine
|
|
gptkbp:type
|
radial engine
|
|
gptkbp:weight
|
150 lb
|