Articulo de referencia

Boeing XP-15

Angelucci 1987, pp. 81-82. XF5B-1 - February 1930 Angelucci 1987, pp. 81-82. "},"introduction":{"wt":""},"retired":{"wt":""},"status":{"wt":"XP-15 - Destroyed"},"primary_user":{...

The Boeing XP-15 was an American prototype monoplanefighter.

Design and development

This aircraft was essentially a monoplane version of the Boeing P-12, differing in having the lower wing omitted and in having all-metal construction as well as altered ailerons. The XP-15 had a split-axle undercarriage and a tail wheel.[1]

Boeing numbered the craft as its Model 202; while the United States Army accepted it for testing and designated it as XP-15, they never actually purchased it, and it retained its civil registration of X-270V.[1]

Operational history

The XP-15 first flew in January 1930, when it was discovered that the vertical stabilizer (a P-12C type) needed to be larger in order to compensate for the single wing. Initial testing showed a top speed to 178 mph, but with enlarged tail surfaces and a Townend cowling, it recorded 190 mph at 8,000 ft. The aircraft performed poorly, with a poor rate of climb and a high landing speed. The USAAC did not order the aircraft for production and on 7 February 1931, the prototype was destroyed when a propeller blade failed and the engine tore loose from its mounts.[1]

The Navy was offered the similar Model 205. It first flew in February 1930. One was bought by the US Navy as the XF5B-1, but by the time flight testing was complete in 1932, other aircraft were ordered instead.

Variants

XP-15
1 built
XF5B-1
1 built

Operators

The XF5B-1
United States

Specifications (XP-15)

Data from Angelucci 1987, pp. 81–82.[1]

General characteristics

  • Crew: one
  • Length: 21 ft 0 in (6.40 m)
  • Wingspan: 30 ft 6 in (9.29 m)
  • Height: 9 ft 4.5 in (2.84 m)
  • Wing area: 157.3 sq ft (14.61 m2)
  • Empty weight: 2,052 lb (931 kg)
  • Gross weight: 2,746 lb (1,246 kg)
  • Powerplant: 1 × Pratt & Whitney SR-1340D Wasp , 525 hp (391 kW)

Performance

  • Maximum speed: 190.2 mph (306 km/h, 165.3 kn)
  • Cruise speed: 160 mph (257 km/h, 140 kn)
  • Alcance: 420  mi (676  km, 360  nmi)
  • Techo de servicio: 27.650  pies (8.428  m)
  • Velocidad de ascenso: 1800  pies/min (9,15  m/s)

Armamento

  • 2 ametralladoras de calibre .30

Véase también

Desarrollo relacionado

Listas relacionadas

Referencias

Notas

  1. ^ Angelucci 1987 , págs . 81-82 .

Bibliografía

  • Angelucci, Enzo. El caza americano desde 1917 hasta la actualidad . Nueva York: Orion Books, 1987.
  • Jones, Lloyd S. Aviones de combate estadounidenses, Ejército-Fuerza Aérea: 1925 a la década de 1980. Fallbrook, California: Aero Publishers Incorporated, 1975, págs.  48-49. ISBN 0-8168-9200-8.