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词条 Loening PW-2
释义

  1. Development

  2. Variants

  3. Operators

  4. Specifications (PW-2A)

  5. See also

  6. References

name=Loening PW-2image=Loening PW-2 Ray Wagner Collection (16004092984).jpgcaption=

}}{{Infobox Aircraft Type

type=Monoplane fighternational origin=United Statesmanufacturer=Loening Aeronautical Engineeringdesigner=Grover Loeningfirst flight=1920introduced=retired=status=primary user=United States Army Air Corpsmore users=produced=number built=7developed from=Loening M-8variants with their own articles=
}}

The Loening PW-2 was a 1920s American single-seat fighter monoplane designed by Grover Loening and built by his Loening Aeronautical Engineering Company.

Development

Based on the earlier two-seat braced-wing monoplane fighter, the M-8, the PW-2 was a single-seat variant for the United States Army Air Corps. It had a fixed tailskid landing gear and was powered by a nose-mounted Wright-Hispano H engine with a tractor propeller. The pilot had an open cockpit. The company built three prototypes designated the PW-2 and a production order for 10 aircraft designated the PW-2A followed. The PW-2As were similar to the PW-2 but had a revised tail unit. After four aircraft had been delivered, one aircraft crashed when the wings separated from the aircraft; the contract was canceled. One of the PW-2As was modified with shorter-span wings and a {{convert|350|hp|kW|lk=on|abbr=on}} Packard 1A-1237 engine as the PW-2B.

Variants

PW-2

Prototype, three built one of which had twin rudders and was not flown and used for static testing.

PW-2A

Production variant with revised tail unit, four built and six cancelled.

PW-2B

PW-2A variant with shorter span wings and a 350hp (261kW) Packard 1A-1237

Operators

{{USA}}

United States Army Air Corps

Specifications (PW-2A)

{{aerospecs
|ref=Fighters of the United States Air Force [1]
|met or eng?=eng
|crew=1
|capacity=
|length m=7.95
|length ft=26
|length in=1
|span m=12.12
|span ft=39
|span in=9
|height m=
|height ft=
|height in=
|wing area sqm=27.8
|wing area sqft=299[2]
|empty weight kg=
|empty weight lb=
|gross weight kg=1270
|gross weight lb=2799
|eng1 number=1
|eng1 type=Wright-Hispano H engine
|eng1 kw=239
|eng1 hp=320
|max speed kmh=219
|max speed mph=136
|cruise speed kmh=
|cruise speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|climb rate ms=
|climb rate ftmin=
|armament1=2 × {{convert|.30|in|mm|2|abbr=on}} Lewis machine guns
}}

See also

{{aircontent
|see also=
|related=
  • Loening M-8

|similar aircraft=
|sequence=
|lists=
  • List of military aircraft of the United States

}}

References

{{commons category|Loening}}
Notes
1. ^Dorr and Donald 1990, p.25.
2. ^Swanborough and Bowers 1962, p.519.
Bibliography
{{refbegin}}
  • {{cite book |last= Andrade |first= John |title= U.S.Military Aircraft Designations and Serials since 1909|year=1979 |publisher=Midland Counties Publications|isbn= 0-904597-22-9}}
  • {{cite book |title= Fighters of the United States Air Force|last=Dorr |first= Robert F.| authorlink= |author2=Donald, David |year= 1990|publisher=Aerospace Publishing |location= London| isbn= 0-600-55094-X|pages= }}
  • {{cite book |title= United States Military Aircraft since 1909|last= Swanborough|first= F.G.| authorlink= |author2=Bowers, Peter M. |year= 1963|publisher=Putnam |location=London |isbn= |pages = }}
  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }}
  • {{cite book |last= |first= |authorlink= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing|location= |issn=|pages=2376}}
{{refend}}{{Loening aircraft}}{{USAAS fighters}}{{DEFAULTSORT:Loening PW-02}}

2 : United States fighter aircraft 1920–1929|Loening aircraft

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