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Curtiss F6C Hawk

From Wikipedia, the free encyclopedia
Late 1920s American naval biplane fighter aircraft
For the Honda motorcycle called F6C in Europe, seeHonda Valkyrie.
F6C Hawk
Curtiss F6C-1 - Model 34
General information
TypeCarrier-borne or land-based fighter
ManufacturerCurtiss Aeroplane and Motor Company
Primary usersUnited States Navy
Number built75
History
Manufactured1927
Introduction date1925

TheCurtiss F6C Hawk is a late 1920sAmerican navalbiplanefighter aircraft. It was part of the long line ofCurtiss Hawk airplanes built by theCurtiss Aeroplane and Motor Company for the American military.

Originally designed for land-based use, theModel 34C was virtually identical to theP-1 Hawk inUnited States Army Air Corps service. TheUnited States Navy ordered nine, but starting with the sixth example, they were strengthened forcarrier-borne operations and redesignatedModel 34D. Flown from the carriersLangley andLexington from 1927–30, most of the later variants passed toMarine fighter-bomber units, while a few were flown for a time as twin-floatfloatplanes.

Operators

[edit]
  •  United States
    • VF-9M (US Marines) operated 5Model 34C,F6C-1 andXF6C-4 from land bases.
    • VF-2 (US Navy) operated 4Model 34D,F6C-2 fromLangley
    • VF-5S, later renamed VF-1B (US Navy) along with VF-8M (US Marines) operated 35Model 34E,F6C-3 fromLexington
    • VF-2B (US Navy) operated 31Model 34H,F6C-4 fromLangley

Variants

[edit]
F6C racing plane.
The XF6C-6
  • F6C-1Model 34C virtually identical to the P-1 series.
  • F6C-2Model 34D strengthened for carrierborne operations and fitted with arrester hooks.
  • F6C-3Model 34E modified version of the F6C-2.
  • XF6C-4Model 34H prototypeF6C-1 with aPratt & Whitney R-1340 Waspradial engine.
  • F6C-4Model 34H production version of theXF6C-4.
  • XF6C-5Model 34H prototypeF6C-1 with aPratt & Whitney R-1690 Hornet radial of 525 hp (391 kW).
  • F6C-6Model 34E modified for racing, with itsradiator located inside thefuselage.
  • XF6C-6Model 34E theF6C-6 which had won the 1930Curtiss Marine Trophy was converted to parasol-wingmonoplane configuration and given wing surface radiators; after achieving the fastest lap in the 1930Thompson Trophy race the XF6C-6 crashed when its pilot was overcome by fumes.[1]
  • XF6C-7Model 34H testbed for an experimental 350 hp (260 kW)Ranger SGV-770C-1 air-cooled inverted Vee engine.

Specifications (F6C-4)

[edit]
Curtiss F6C-4 3-view drawing from L'Aéronautique October,1927

Data from United States Navy Aircraft since 1911[2]

General characteristics

  • Crew: 1
  • Length: 22 ft 6 in (6.86 m)
  • Wingspan: 37 ft 6 in (11.43 m)
  • Height: 10 ft 11 in (3.33 m)
  • Wing area: 252 sq ft (23.4 m2)
  • Airfoil: Clark Y[3]
  • Empty weight: 1,980 lb (898 kg)
  • Max takeoff weight: 3,171 lb (1,438 kg)
  • Powerplant: 1 ×Pratt & Whitney R-1340 Wasp 9-cylinder air-cooled radial piston engine, 410 hp (310 kW)
  • Propellers: 2-bladed metal propeller

Performance

  • Maximum speed: 155 mph (249 km/h, 135 kn) at sea level
  • Range: 360 mi (580 km, 310 nmi)
  • Service ceiling: 22,900 ft (7,000 m)
  • Time to altitude: 5,000 ft (1,500 m) in 2 minutes 30 seconds

Armament

See also

[edit]

Related development

References

[edit]
Wikimedia Commons has media related toCurtiss F6C Hawk.
  1. ^Pearce, William (25 February 2015)."Curtiss XF6C-6 Navy Racer".oldmachinepress.com. Retrieved17 May 2016.
  2. ^Swanborough and Bowers 1976, p. 130.
  3. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.
  • Eden, Paul and Soph Moeng.The complete Encyclopedia of World Aircraft. London:Amber Books, 2002.
  • Swanborough, Gordon and Peter M. Bowers.United States Navy Aircraft since 1911. London:Putnam, Second edition, 1976.ISBN 0-370-10054-9.
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See also:Aeromarine AS  • Vought VE-7
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