About: Fisher P-75 Eagle   Sponge Permalink

An Entity of Type : dbkwik:resource/2mp-WpdlZ802dyt7T6jpKA==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The General Motors/Fisher P-75 Eagle was a fighter aircraft designed by the Fisher Body Division of General Motors Corporation. Development started in September 1942 in response to United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb, using the most powerful liquid-cooled engine then available, the Allison V-3420. The program was cancelled after only a small number of prototypes and production aircraft had been completed, as it was no longer required in its original role, could not be quickly deployed, and possessed no significant advantages over aircraft already in production.

AttributesValues
rdf:type
rdfs:label
  • Fisher P-75 Eagle
rdfs:comment
  • The General Motors/Fisher P-75 Eagle was a fighter aircraft designed by the Fisher Body Division of General Motors Corporation. Development started in September 1942 in response to United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb, using the most powerful liquid-cooled engine then available, the Allison V-3420. The program was cancelled after only a small number of prototypes and production aircraft had been completed, as it was no longer required in its original role, could not be quickly deployed, and possessed no significant advantages over aircraft already in production.
  • The Fisher P-75 Eagle was an interceptor aircraft developed to meet an urgent USAAF requirement.
sameAs
Length
  • 1259.8400000000001
fullweight
  • 19420.0
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
dbkwik:world-war-2...iPageUsesTemplate
max takeoff weight alt
  • 8260.0
loaded weight main
  • 19420.0
Range
  • 2150.0
max speed more
  • at 20,000
climb rate main
  • 4200.0
number of props
  • 1(xsd:integer)
length alt
  • 12.32 m
span main
  • 1503.68
emptyweight
  • 11255.0
Speed
  • 400(xsd:integer)
power/mass alt
  • 0(xsd:double)
Status
  • --10-06
Affiliation
Role
  • Interception
height alt
  • 4.72 m
Name
  • Fisher P-75A
  • P-75 Eagle
primary user
Type
  • Fighter
type of prop
  • liquid-cooled 24-cylinder double-Vee
loading main
  • 39(xsd:double)
range alt
  • 3300.0
Caption
  • The first Fisher XP-75-GM, SN 43-46950, in flight.
  • The last production P-75A , now in the USAF Museum in Dayton, OH
Program Cost
  • $50.12 million USD
length main
  • 1231.9
power alt
  • 2150.0
area main
  • 347.0
power main
  • 2885.0
height main
  • 472.44
Wingspan
  • 1503.68
span alt
  • 15.04 m
range main
  • 2050.0
Height
  • 502.92
Manufacturer
  • Fisher Body Division, General Motors Corporation
max speed main
  • 433.0
engine (prop)
  • Allison V-3420-23
power/mass main
  • 0(xsd:double)
climb rate alt
  • 21.3
ceiling main
  • 36400.0
empty weight main
  • 11495.0
loaded weight alt
  • 8808.0
area alt
  • 32.24
First Flight
  • 1943-11-17(xsd:date)
max speed alt
  • 697.0
jet or prop?
  • prop
loading alt
  • 194(xsd:double)
empty weight alt
  • 5214.0
Engine
  • One 24 cylinder V-3240-19, rated at 2,600 hp
plane or copter?
  • plane
ceiling alt
  • 11,100 m
max takeoff weight main
  • 18210.0
Crew
  • 1(xsd:integer)
  • One
Armament
  • Ten .5 in Machine gunsref|Of these, four would be mounted in the fuselage, and synchronished to fire between the prop blades. The remaining six would be unsynchronised, and mounted in the wings.|group="N"
  • * 6x .50 caliber wing mounted machine guns * 4x .50 caliber fuselage mounted machine guns * 2x 500 lb bombs
Number Built
  • 13(xsd:integer)
Year
  • 1943(xsd:integer)
Designer
ref
  • and
abstract
  • The General Motors/Fisher P-75 Eagle was a fighter aircraft designed by the Fisher Body Division of General Motors Corporation. Development started in September 1942 in response to United States Army Air Forces requirement for a fighter possessing an extremely high rate of climb, using the most powerful liquid-cooled engine then available, the Allison V-3420. The program was cancelled after only a small number of prototypes and production aircraft had been completed, as it was no longer required in its original role, could not be quickly deployed, and possessed no significant advantages over aircraft already in production.
  • The Fisher P-75 Eagle was an interceptor aircraft developed to meet an urgent USAAF requirement.
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