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词条 Armstrong Whitworth Wolf
释义

  1. Design and development

  2. Operators

  3. Specifications (Wolf)

  4. See also

  5. Notes

  6. References

{{Use dmy dates|date=August 2017}}{{Use British English|date=August 2017}}
name=Wolfimage=AWWolf.jpgcaption=

}}{{Infobox Aircraft Type

type=Trainermanufacturer=Armstrong Whitworth Aircraftdesigner=first flight=19 January 1923introduced=1923retired=1931status=primary user=Royal Air Forcemore users=Royal Aircraft Establishmentproduced=1923-1929number built=6variants with their own articles=
}}

The Armstrong Whitworth Wolf was a British two-seat reconnaissance aircraft ordered by the Royal Air Force in 1923.

Design and development

The Wolf was a two-bay biplane of unorthodox design, with the fuselage mounted between the two sets of wings. No production order was placed, and the three machines built served their days at the Royal Aircraft Establishment at Farnborough as experimental testbeds.

Alongside the RAF's order in 1923, Armstrong Whitworth also built two for the RAF Reserve Flying School at Whitley, and a final, sixth aircraft in 1929. As trainers, they proved popular with pilots, although less so with ground crews for whom the rigging and undercarriage were awkward to maintain.

All Wolves were retired from service in 1931 and all but the most recently built were scrapped. The final aircraft was taken to Hamble for use as an instructional airframe.

Operators

{{UK}}
  • Royal Air Force
  • Royal Aircraft Establishment

Specifications (Wolf)

{{Aircraft specs
|ref=Armstrong Whitworth Aircraft since 1913 [1]
|prime units?=imp


|genhide=
|crew=2[2]
|capacity=
|length m=
|length ft=31
|length in=0
|span m=
|span ft=39
|span in=10
|height m=
|height ft=13
|height in=0
|wing area sqm=
|wing area sqft=488
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=2690
|empty weight note=
|gross weight kg=
|gross weight lb=4090
|gross weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Armstrong Siddeley Jaguar III
|eng1 type=14-cylinder two-row air-cooled radial engine
|eng1 kw=
|eng1 hp=350
|power original=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=110
|max speed kts=
|max speed note=at {{convert|10000|ft|m|abbr=on}}
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|range km=
|range miles=
|range nmi=
|endurance=3 hr 45 min
|ceiling m=
|ceiling ft=15150
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|time to altitude=

  • 1.3 min to {{convert|1000|ft|m|abbr=on}}
  • 6.5 min to {{convert|5000|ft|m|abbr=on}}

|more performance=


|guns=[2]

  • 1 × fixed, forward-firing .303 in (7.7 mm) Vickers machine gun
  • 1 × .303 in (7.7 mm) Lewis Gun in Scarff ring for observer

|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}

See also

{{aircontent
|related=
|similar aircraft=
|lists=
  • List of aircraft of the Royal Air Force

|see also=
}}

Notes

1. ^Tapper 1988, p.151.
2. ^Tapper 1988, p. 143.

References

{{commons category|Armstrong Whitworth Wolf}}
  • {{cite book |last=Tapper |first=Oliver |authorlink= |title=Armstrong Whitworth Aircraft since 1913 |year= 1988|publisher= Putnam|location=London |isbn=0-85177-826-7 |page= |pages= |url= |accessdate=}}
  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=81 }}
  • {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 889 Sheet 80 }}
{{Armstrong Whitworth aircraft}}

5 : British military reconnaissance aircraft 1920–1929|Armstrong Whitworth aircraft|Biplanes|Single-engined tractor aircraft|Aircraft first flown in 1923

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