켈렛 K-2 | |
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국가 | 미국 |
역할 | 유틸리티 오토자이로 |
첫 비행 | 1931년 4월 24일 |
내장 | 16 |
Tthe 켈렛 K-2 는 1930년대 초 미국에서 개발된 두 좌석 오토자이로였다. 나중에 더 강력한 엔진을 장착 할 때 K-3 및 K-4로 지정되었습니다.
소스: 켈렛 K-2 위키백과에
켈렛 K-2 산책 | |
---|---|
사진 작가 | 블라디미르 야쿠보프 |
로컬라이제이션 | USAF 국립 박물관 |
사진 | 47 |
관련 키트:
이베이에서 키트 찾기:
The Kellett 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 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.
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