avia.wikisort.org - Aeroplane

The Cox-Klemin TW-2 was a 1920s American biplane training aircraft built by the Cox-Klemin Aircraft Corporation. It was powered by a water-cooled Hispano-Suiza 8 V8 aero-engine.

Cox-Klemin TW-2
Role	Biplane trainer Type of aircraft
Manufacturer	Cox-Klemin Aircraft Corporation
First flight	1921
Primary user	United States Army Air Corps
Number built	3

Development

The CK-2 was a biplane with single-bay biplane that utilized a Fokker scheme of N-shaped interplane struts and metal cabane. Three aircraft were built, two flight articles that were used to test different engines and one static test article. However, the TW-2 was not ordered into production.[1][2]

Operators

 United States

• United States Army Air Service

Specifications

General characteristics

• Crew: 2
• Length: 23 ft (7.0 m)
• Wingspan: 29 ft (8.8 m)
• Gross weight: 2,505 lb (1,136 kg)
• Powerplant: 1 × Wright Hispano E V-8 liquid-cooled piston engine, 180 hp (130 kW)
• Propellers: 2-bladed fixed-pitch pusher propeller

Performance

• Maximum speed: 99 mph (159 km/h, 86 kn)

See also

Related lists

• List of military aircraft of the United States

References

• Andrade, John. U.S. Military Aircraft Designations and Serials since 1909. Midland Counties Publications, 1979; page 171. ISBN 0-904597-22-9.

На других языках

---

[de] Cox-Klemin TW-2

Die Cox-Klemin TW-2 war ein Trainingsflugzeug der Cox-Klemin Aircraft Corporation von 1921 für den United States Army Air Service. Es wurden drei Maschinen gebaut.[1]

---

- [en] Cox-Klemin TW-2

---

[fr] Cox-Klemin TW-2

Le Cox-Klemin TW-2 était un avion militaire de l'entre-deux-guerres, construit aux États-Unis par la Cox-Klemin Aircraft Corporation.

---

---