Kayaba Ku-3: Difference between revisions
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Revision as of 20:49, 17 November 2017
| Ku-3 | |
|---|---|
| |
| Role | Research glider |
| National origin | Japan |
| Manufacturer | Kayaba Industry |
| Designer | Hidemasa Kimura and Joji Washimi |
| First flight | February Template:Avyear |
| Number built | 1 |
The Kayaba Ku-3 was a glider built in Japan in 1941 to investigate the possibilities of tailless aircraft. Building on the success of the Ku-2 design of the previous year, the Ku-3 was a substantially larger aircraft with several novel features. The small vertical fins of the Ku-2 were abandoned, leaving the Ku-3 with no vertical control surfaces. The wing was a cranked delta design, with three pairs of control surfaces on the trailing edge. The outer, less-swept wing sections had a greater dihedral than the inner sections.
The prototype crashed after 67 flights, when the test pilot was unable to recover from a spin.
General characteristics Performance
References
- Wooldridge, E.T. "Japanese flying wings". History of the Flying Wing. Retrieved 29 April 2007.
- 日本飞翼的短暂研究