Navy-Wright NW

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NW Mystery Racer
Navy-Wright NW-1 Mystery Ship.jpg
The NW-1 before going to Selfridge Field, Michigan, 1922
Role Air racing
National origin United States
Manufacturer Wright Aeronautical Corporation
Designer Rex Beisel [1]
First flight11 October 1922 [2]
StatusBoth aircraft destroyed
Primary user US Navy
Number built2 (2 NW-1, 1 NW-2 (rebuilt from the original NW-1)

The Navy-Wright NW series, also called the Mystery Racer were racing aircraft built by Wright Aeronautical Corporation at the request of the US Navy. Although innovative, both prototype racers were lost before achieving their true potential.

Contents

Design and development

In the early 1920s, the US Navy asked the Wright Aeronautical Corporation to design an engine based on the Lawrance J-1, the result being the Wright T-2 12-cylinder, water-cooled engine, with a proposed horsepower rating of 650 hp. At the time there was no aircraft that could properly use the engine, so the US Navy Bureau of Aeronautics designed an airframe to accommodate the new powerplant with construction of two prototypes (BU. Aer. Nos. A-6543 and A-6544) undertaken by the Wright Corporation. [1]

Designated the Navy-Wright NW-1, A-6543, the first prototype was designed and built in three months, and flew for the first time on 11 October 1922, just days before it was entered in the 14 October 1922 Pulitzer air race at Selfridge Field, Michigan. Entered at the last minute, the press dubbed the new entry, the Mystery Racer. [3]

The Navy-Wright NW-1 was an unconventional streamlined design, based on a sesquiplane with main wheels faired into the lower wing, and bracing minimized to further reduce drag. Lamblin radiators were suspended beneath the fuselage and wire bracing was incorporated for the mid-fuselage mounted main wing and tailplane. [4]

Operational history

With the rush to complete the NW-1, the aircraft was not fully tested and by the time of the Pulitzer Race, Lt. S. Sanderson had little opportunity to fly the racer. During the race, the NW-1 wearing race number "9", although reaching a top speed of 186 mph, its engine overheated and failed causing the NW-1 to ditch into Lake St. Clair, flipping over on its back. [4]

Navy-Wright NW-2 during testing at Cowes, Isle of Wight, 1923 Navy-Wright NW-2 ile de Wight.jpg
Navy-Wright NW-2 during testing at Cowes, Isle of Wight, 1923

Extensive changes

With the major damage suffered in the ditching, the US Navy resorted to cannibalizing the wrecked aircraft to provide spares for the second prototype, A-6544, which had been retained as an engine testbed for the T-2 engine. [5]

Early in 1923, a decision was made to redesign the racer and in the months following, a completely new design emerged with the original landplane being converted into a floatplane. Radical surgery was performed to turn the sesquiplane into a biplane, with strutted wings, wing surface radiators, enlarged tail surfaces and a set of floats also part of the redesign. Fitted with a new, more powerful 700 hp Wright T-3, a development of the T-2 and a three-blade propeller, the second of the NW series was designated NW-2 and was entered into the 1923 Schneider Trophy held at Cowes, Isle of Wight. [4]

The Navy conducted flight testing at Anacostia achieving a top speed of 176 mph, before shipping the NW-2 to England in September 1923. At Cowes, wearing the race number "5", during pre-race testing, the NW-2 suffered a propeller failure in flight with the shattered propeller slicing into the floats. The pilot, Lt. Frank Wead alighted but the severely damaged floats collapsed and the NW-2 sank, with Wead scrambling to safety, and being rescued uninjured. [6]

The Navy-Wright NW series was abandoned after the sinking of the NW-2.

Operators

Flag of the United States (23px).png  United States

Specifications (NW-1)

Data from [4]

General characteristics

Performance

Specifications (NW-2)

Data from [4]

General characteristics

Performance

See also

Aircraft of comparable role, configuration, and era

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References

Notes
  1. 1 2 Cowin 1999, p. 26.
  2. Angelucci 1987, pp. 325–326.
  3. 1 2 Kinnert 1969, p. 70.
  4. 1 2 3 4 5 6 Cowin 1962, p. 361.
  5. Kinnert 1969, p. 67.
  6. Kinnert 1969, p. 78.
Bibliography