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Robertson Skylark SRX-1 : ウィキペディア英語版 | Robertson Skylark SRX-1
The Robertson Skylark SRX-1 is a five place high performance STOL aircraft designed in the 1950s. It was intended to operated out of landing strips with cruise speeds.
==Design== The aircraft was designed by James L. Robertson, son of William B. Robertson, Robertson Aircraft Corporation founder at the age of 27. The aircraft is designed to be stall-proof and spin-proof and is capable of a minimum flight speed. It was also the first light aircraft in America to be designed to accommodate a turboprop engine. The Skylark is all metal, with a steel tube internal structure. It incorporates shrouds, flaps, spoilerons, turbulator control, stabilators, elevances, and spinner duct cooling.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Robertson Skylark SRX-1」の詳細全文を読む
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