|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
air superiority
military aircraft
straight wing
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:built
|
50
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:constructionMaterial
|
aluminum
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:covers
|
split flaps
|
|
gptkbp:crew
|
1
|
|
gptkbp:decommissioned
|
1950
|
|
gptkbp:design
|
gptkb:William_C._Wright
|
|
gptkbp:design_feature
|
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:Wright_R-1300
|
|
gptkbp:engineType
|
radial engine
|
|
gptkbp:firstFlight
|
1941
|
|
gptkbp:floors
|
conventional tail
|
|
gptkbp:fuel_capacity
|
200 gallons
|
|
gptkbp:hasExperienceIn
|
500 miles
|
|
gptkbp:height
|
10 ft 0 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright Model V-4
|
|
gptkbp:influenced
|
gptkb:Wright_Model_V-3
|
|
gptkbp:inspiration
|
performance-oriented design
|
|
gptkbp:introduced
|
1942
|
|
gptkbp:inventor
|
V-4A
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced future fighter designs
|
|
gptkbp:length
|
30 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:maximum_speed
|
350 mph
|
|
gptkbp:maxTakeoffWeight
|
5,000 lb
|
|
gptkbp:notable_feature
|
high speed and agility
|
|
gptkbp:operationalHistory
|
served_in_World_War_II
|
|
gptkbp:operationalStatus
|
frise ailerons
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:primaryUser
|
gptkb:United_States_Air_Force
|
|
gptkbp:productionYears
|
1941-1945
|
|
gptkbp:propulsion
|
variable pitch propeller
|
|
gptkbp:range
|
1,000 miles
|
|
gptkbp:retirementYear
|
advancements in technology
|
|
gptkbp:role
|
interceptor
|
|
gptkbp:safety_features
|
limited radar cross-section
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:status
|
retired
|
|
gptkbp:steering
|
vertical stabilizer
|
|
gptkbp:successor
|
gptkb:Wright_Model_V-5
|
|
gptkbp:surrounding_area
|
250 sq ft
|
|
gptkbp:team
|
Wright_Aeronautical_engineers
|
|
gptkbp:trainTypes
|
gptkb:V-4B
|
|
gptkbp:type
|
fighter aircraft
|
|
gptkbp:wingspan
|
36 ft 0 in
|