United States (1928)
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Only a single example of the experimental Boeing XP-8 pursuit fighter was ever produced.
Detailing the development and operational history of the Boeing XP-8 Prototype Fighter. Entry last updated on 4/25/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com
The Boeing XP-8 represented a "one-off" biplane fighter prototype (Boeing Model 66). It continued use of a biplane wing arrangement as well as open-air cockpit and fixed undercarriage structure. The airframe was powered by a single, front-mounted Packard engine and carried its radiator system along the lower wing root - a distinct feature in its design. The aircraft was further distinguished by its noticeably contoured nose assembly which was to aid in aerodynamic efficiency at expected speeds. Armament was consistent with aircraft of the time and made up of a combination of 1 x 0.30 caliber medium machine gun and 1 x 0.50 caliber heavy machine gun in fixed mountings for forward-firing. Power was served through a single Packard 2A-1530 series inverted "vee" engine delivering 600 horsepower allowing the XP-8 a top listed speed of 170 miles per hour while cruising was around 135 miles per hour. The aircraft displayed a service ceiling of 20,950 feet and range of 325 miles. Rate-of-climb was a useful 1,750 feet per minute. The engine drove a two-bladed propeller assembly. Dimensionally, the XP-8 showcased a length of 23 feet, 4 inches, a wingspan of 30 feet and a height of 8 feet, 4 inches. Maximum weight was listed at 3,420 lbs. The main wings were of uneven span featuring parallel struts and cabling with the pilot seated aft and under the upper wing arrangement.
The aircraft was delivered USAAC testing facilities in early 1928. Pilots noted the type's good handling characteristics thought he test vehicle could not attained required speeds for an Army fighter. Engine problems soon developed where engine oil and water would leak into the bottom of the powerplant and foul sparkplugs. The issue was never resolved and, despite evaluation into June of 1929, the aircraft was not accepted for Army service. The prototype was then scrapped and lost to history though Boeing utilized some qualities of the design to sell the US Navy, Japan and Brazil on its F2B model - 33 built in all.
Any available statistics for the Boeing XP-8 Prototype Fighter are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
This entry's maximum listed speed (176mph).
Graph average of 150 miles-per-hour.
Graph showcases the Boeing XP-8's operational range (on internal fuel) when compared to distances between major cities.