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Fisher XP-75 / P-75 Eagle Interceptor (1943)

Authored By Staff Writer | Last Updated: 4/29/2015

Unfortunately for the Fisher XP-75 Eagle, it fulfilled a requirement no longer needed by the United States Army Air Forces.

General Motors became a major player in the American manufacturing realm when World War 2 arrived for the United States. With its automotive plants adept at mass-production, it was only fitting that the US military look to such institutions for production of such war implements as bullets, guns, tanks and - of course - aircraft. General Motors made an easy conversion to production for the new orders (both foreign and domestic) and had already developed a hand in the aircraft industry with the ownership of the Allison engine company.

Allison was a key supplier of aircraft engines to the US Army and took to development of a new series product under the designation of V-3420, developed from the mating of two V-1710 series engines. In theory it was a vastly powerful engine but it remained wholly untested in the real world war time market. Nevertheless, a new product warranted equally new sales for the division and General Motors was not going to let its new engine development lay by the wayside - not with a world war going on.

By 1942, development of the war was not without its growing pains for the US military. Though it was already putting together a successful stead of legendary "pursuit" fighters in the North American P-51 Mustang, the Republic P-47 Thunderbolt and the Lockheed P-38 Lightning, these aircraft would generally not reach their true pinnacles for a few more years to come. As such, the need was apparent for better performing, high-flying and lethal interceptors to help stave off any aerial advantage that lay in the German Luftwaffe to this point. As such, a fighter needed to be developed that could provide a lethal punch against both fighter or bomber and could respond to incoming threats through excellent climbing abilities and top speed.

General Motors saw this as the perfect opportunity to showcase the new Allison powerplant and moved to convert their Fisher Body Plant in Cleveland, Ohio for production of not only the Allison engine but also of a new interceptor to fill the US Army need. Accordingly, they penciled out a design specifically fitting their powerplant and submitted it for review. Amazingly, the US Army took notice and accepted the General Motors idea - moreso in terms that the new fighter could be rapidly produced while fulfilling the performance requests as needed by the Army. The contract called for two complete prototypes and the designation of XP-75 was assigned.

To keep design and development of the new system short, the idea presented was to build an aircraft out of proven portions of existing airframes with the entire concoction fitted around the Allison V-3420. Outer wing surfaces were pulled from a P-51 Mustang while the wings themselves were originally slated to resemble the inverted "gull wing" implements as found on the Vought F4U Corsair fighter. The inverted gull wings were dropped from the design and, instead, the wings of a Curtiss P-40 Warhawk was used in its place though the undercarriage of the F4U was still selected for use. The empennage was to be made up from the system of a Douglas Dauntless dive bomber.

The final result became one of the most unique - if not dysfunctional-looking - aircraft designs to emerge from World War 2. The fuselage became a long slender affair with the cockpit situated quite well-ahead of the low-mounted monoplane wings. The nose protruded out some and was capped with a contra-rotating set of three-bladed propellers (giving the appearance of six blades in the nose). The design called for the Allison powerplant to be fitted at the midway point of the fuselage with a drive shaft running under the cockpit floor and attached to each propeller system. As a liquid-cooled engine, the V-3420 had no need for air cooling scoops and could be fitted as such. The radiator was fed via two scoops mounted under the rearward portion of the fuselage. The empennage maintained curved surface features and was topped with a smallish sort of vertical tail fin and accompanying horizontal planes. The undercarriage consisted of two main landing gears - one mounted under each wing - and a diminutive tail wheel. The canopy was heavily framed at first and offered up adequate views all-around the airframe. In whole, the XP-75 was constructed over in all-metal stressed skin.


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Specifications for the
Fisher XP-75 / P-75 Eagle
Interceptor


Focus Model: Fisher P-75A Eagle
Country of Origin: United States
Manufacturer: General Motors (Fisher Plant) - USA
Initial Year of Service: 1943
Production: 14


Crew: 1


Length: 41.31 ft (12.59 m)
Width: 49.31 ft (15.03 m)
Height: 15.49ft (4.72 m)
Weight (Empty): 11,255 lb (5,105 kg)
Weight (MTOW): 19,418 lb (8,808 kg)


Powerplant: 1 x Allison V-3420-23 generating 2,600hp.


Maximum Speed: 404 mph (650 kmh; 351 kts)
Maximum Range: 1,150 miles (1,850 km)
Service Ceiling: 40,000 ft (12,192 m; 7.6 miles)
Rate-of-Climb: 4,200 feet-per-minute (1,280 m/min)


Hardpoints: 0
Armament Suite:
Proposed but never fitted:

6 x 12.7mm machine guns in wings
4 x 12.7mm machine guns in upper forward fuselage


Variants:
XP-75-GM - Composite Design Prototypes S/N 43-46950 and S/N 43-46951.


XP-75A-GC - Production Prototypes; S/N 44-44549 through 44-44554; 6 examples produced.

P-75A - Limited Production Model Designation for US Army; 6 examples produced; 2,494 examples cancelled.


Operators:
United States