凯利特K-2 | |
|---|---|
| 国家 | 美国 |
| 作用 | 实用自动陀螺仪 |
| 首次飞行 | 1931年4月24日 |
| 建立 | 16 |
这 凯利特K-2 是20世纪30年代初在美国开发的双座自动陀螺仪。后来的例子被指定为K-3和K-4时，配备了更强大的发动机。
源： 维基百科上的凯利特K-2
| 凯莱特 K - 2 四处走动 | |
|---|---|
| 摄影师 | 弗拉基米尔·亚库博夫 |
| 本地化 | 美国空军国家博物馆 |
| 照片 | 47 |
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这 凯利特K-2 was an autogyro developed in the United States in the 1930s. It was a two-seat aircraft with an open cockpit and a conventional tailwheel landing gear. The rotor was powered by a small engine mounted on the mast, while the main engine drove a propeller in the nose. The K-2 was designed for civil and military use, and was tested by the US Army Air Corps as a possible observation and liaison aircraft.
The K-2 had a low stall speed and could take off and land in short distances, making it suitable for operation from unprepared fields. However, it also had some drawbacks, such as limited forward speed, high fuel consumption, and vulnerability to crosswinds. The K-2型 was not adopted by the military, but some were sold to private owners and used for various purposes, such as aerial photography, crop dusting, and barnstorming.
视图 ： 806
