Verville VCP

{{Infobox Aircraft Begin

|name=VCP-1

|image=Verville Vcp-1.jpg

|caption=

}}{{Infobox Aircraft Type

|type=USAAS Pursuit prototype

|manufacturer=Engineering Division

|designer=Alfred V. Verville

|first flight=11 June 1920

|introduced=

|retired=

|status=

|primary user=

|more users=

|produced=

|number built=2

variants with their own articles =Verville-Packard R-1

}}

The Verville VCP was an American single-engined biplane fighter aircraft of the 1920s. A single example of the VCP-1 was built by the United States Army Air Service's Engineering Division, which was later rebuilt into a successful racing aircraft, while a second, modified fighter was built as the PW-1.

Design and development

=VCP-1=

In 1918, Virginius E. Clark, in charge of the Plane Design section of the U.S. Army Air Service's Engineering Division and Alfred V. Verville, who had recently joined the Engineering Division from private industry, started design of a single-seat fighter (known as "pursuit" aircraft to the U.S. Army), the VCP-1 (Verville-Clark Pursuit).Angelucci and Bowers 1987, p. 197.

Drawing from the experience of the French and their SPAD S.XIII, the desire was to make a sleeker and more maneuverable fighter.Boyne 2001, p. 8. The VCP-1 was powered by a Wright-built {{convert|300|hp|kW|lk=on|abbr=on}} Hispano-Suiza 8 V-8 engine and had tapered single-bay biplane wings. The fuselage was a monocoque structure constructed of plywood, while the wings were of wood and fabric construction. The engine was cooled with an unusual annular radiator.Green and Swanborough 1994, p. 193.Boyne 2001, p. 9.

Two were built, but only one was flown, making its maiden flight on June 11, 1920. The aircraft demonstrated good performance, reaching {{convert|156|mph|km/h|abbr=on}}, but the radical annular radiator was unsuccessful, having to be replaced to a more conventional unit. Because of its performance, it was decided to modify the VCP-1 to a racing aircraft, replacing the Wright-Hispano engine with a {{convert|660|hp|kW|abbr=on}} Packard 1A-2025 V12 engine, becoming the VCP-R (later again rebuilt as the Verville R-1 Racer).Angelucci and Bowers 1987, pp. 197–198.

=PW-1=

In 1920, work commenced on two new fighter aircraft based on the VCP-1, featuring an easier to build fabric covered steel-tube fuselage instead of the plywood monocoque of the VCP-1. The aircraft retained the tapered wings of the VCP-1 and was powered by a {{convert|350|hp|kW|abbr=on}} Packard 1A-1237 engine, cooled by a tunnel-style radiator located under the engine.Angelucci and Bowers 1987, p. 198.Boyne 2001, p. 11.

The new design was initially known as the VCP-2, but was soon redesignated as PW-1 (Pursuit, Water-CooledDorr and Donald 1990, p. 23.) in the U.S. Army Air Service's new designation system. The first aircraft was used for static testing, while the second prototype flew in November 1921, reaching a speed of {{convert|146|mph|km/h|abbr=on}}. It was rebuilt later that year with a new untapered set of wings using a Fokker style thick airfoil, becoming the PW-1A, but performance was reduced, and the aircraft was refitted with its original wings, reverting to the designation PW-1.Dorr and Donald 1990, pp. 24–25.

While plans were prepared for more powerful versions fitted with revised wings, no production ensued.

Operational history

The VCP-R made its racing debut at the 1920 Gordon Bennett Cup race held at Étampes near Paris on 28 September. Its radiator proved to be insufficient to deal with the powerful, high-compression Packard engine, however, and it retired after the first lap.Flight 7 October 1920, pp. 1055–1056. It was taken back to the U.S. and quickly modified with a larger radiator for entry in the Pulitzer Trophy air-race, held at Mineola, New York on 25 November that year. This time it was successful, winning the race at a speed of {{convert|156.5|mph|km/h|1|abbr=on}}.Flight 2 December 1920, p. 1244.

The U.S. Armed Forces did not compete in the 1921 Pulitzer Trophy race,Flight 1 December 1921, p. 805. but for the 1922 race the VCP-R was fitted with a revised tail, becoming the R-1. It finished in sixth place at a speed of {{convert|179|mph|km/h|abbr=on}}.Flight 19 October 1922, pp. 603–605.

Variants

;VCP-1

:Single-seat biplane fighter, powered by 300 hp Wright-Hispano engine. Two built, one flown.

;VCP-R

:Modification of VCP-1 for air-racing, with 660 hp Packard 1A-2025 engine, and capable of reaching a speed of {{convert|177|mph|km/h|abbr=on}}.

;R-1

:Modification of VCP-R for 1922 Pulitzer Trophy race. Maximum speed {{convert|186|mph|km/h|abbr=on}}.

;PW-1

:Modified fighter aircraft with steel-tube fuselage and 350 hp Packard 1A-1237 engine. Two built but only one flown.

;PW-1A

:PW-1 fitted with new, Fokker-style wings. Speed reduced to {{convert|134|mph|km/h|abbr=on}}.Angelucci and Bowers 1987, p. 199.

Specifications (PW-1)

{{Aircraft specs

|ref=The American FighterAngelucci and Bowers 1987, pp. 198–199.

|prime units?=imp

|crew=1

|capacity=

|length m=

|length ft=22

|length in=6

|span m=

|span ft=32

|span in=0

|height m=

|height ft=8

|height in=4

|wing area sqm=

|wing area sqft=269

|airfoil=

|empty weight kg=

|empty weight lb=2069

|gross weight kg=

|gross weight lb=3005

|fuel capacity=

|eng1 number=1

|eng1 name=Packard 1A-1237

|eng1 type=

|eng1 kw=

|eng1 hp=350

|max speed kmh=

|max speed mph=146

|max speed kts=

|max speed note=at sea level

|cruise speed kmh=

|cruise speed mph=132

|cruise speed kts=

|range km=

|range miles=

|range nmi=

|combat range km=

|combat range miles=

|combat range nmi=

|endurance=2 hr 30 min

|ceiling m=

|ceiling ft=19300

|climb rate ms=

|climb rate ftmin=

|time to altitude=11 minutes to 10,000 ft (3,050 m)

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|guns=

|bombs=

|avionics=

}}

References

;Notes

;Bibliography

Angelucci, Enzo and Peter M. Bowers. The American Fighter. Sparkford, UK:Haynes Publishing Group, 1987. {{ISBN|0-85429-635-2}}.
Boyne, Walter J. "The Treasures of McCook Field: America's First Aero Engineering and Testing Centre, Part 1". The Best of Wings Magazine. Washington DC:Brassey's, 2001. pp. 1–9. {{ISBN|1-57488-368-2}}.
Boyne, Walter J. "The Treasures of McCook Field: America's First Aero Engineering and Testing Centre, Part 2". The Best of Wings Magazine. Washington DC:Brassey's, 2001. pp. 10–18. {{ISBN|1-57488-368-2}}.
Dorr, Robert F. and David Donald. Fighters of the United States Air Force. London:Temple Press/Aerospace, 1990. {{ISBN|0-600-55094-X}}.
[http://www.flightglobal.com/pdfarchive/view/1920/1920%20-%201053.html "Gordon-Bennett 1920: The Cup Goes to France"]. Flight, 7 October 1920. pp. 1055–1059.
Green, William and Gordon Swanborough. The Complete Book of Fighters. New York: Smithmark, 1994. {{ISBN|0-8317-3939-8}}.
[http://www.flightglobal.com/pdfarchive/view/1920/1920%20-%201242.html "Reports and Memoranda: The Pulitzer Trophy Race"]. Flight, 2 December 1920, p. 1244.
[http://www.flightglobal.com/pdfarchive/view/1922/1922%20-%200603.html "The 1922 Pulitzer Trophy Race"]. Flight, 19 October 1922, pp. 603–605.
[http://www.flightglobal.com/pdfarchive/view/1921/1921%20-%200805.html "The Second Annual Pulitzer Race at Omaha"]. Flight, 1 December 1921, p. 805.