| Ku-2 | |
|---|---|
 | |
| General information | |
| Type | Research glider |
| National origin | Japan |
| Manufacturer | Kayaba Industry |
| Designer | Hidemasa Kimura |
| Number built | 1 |
| History | |
| First flight | October 1940 |
The Kayaba Ku-2 (萱場 2型無尾翼滑空機) was a glider built in Japan in 1940 to investigate the possibilities of tailless aircraft. It was developed as part of an Imperial Japanese Army contract that had been offered to designer Hidemasa Kimura following the successful flights of his HK-1 tailless glider over the previous years.
Developed with the help of the Kayaba Industry's chief designer Shigeki Naito, the Ku-2 had a swept wing with two vertical fins at the end of the wings. The Ku-2 flew 262 test flights between October 1940 and May 1941 before being damaged beyond repair in a crash.
Specifications
General characteristics
- Crew: One pilot
- Length: 3.04 m (10 ft 0 in)
- Wingspan: 9.80 m (32 ft 2 in)
- Wing area: 14.5 m (156 sq ft)
Performance
- Maximum speed: 75 km/h (47 mph, 41 kn)
References
- Wooldridge, E. T.; National Air and Space Museum (1983). Winged wonders: the story of the flying wings. Washington, DC: Smithsonian Institution Press. p. 85. ISBN 978-0874749663.
- Wooldridge, E.T. "Japanese flying wings". History of the Flying Wing. Retrieved 29 April 2007.
- 日本飞翼的短暂研究 Archived 2012-02-13 at the Wayback Machine
| Kayaba aircraft | |
|---|---|
| Japanese Army Glider Designation System | |
|---|---|