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Schweizer SA 1-30 : ウィキペディア英語版 | Schweizer SA 1-30
The Schweizer SA 1-30 was the first entry by Schweizer in the powered aircraft market. ==Design and development== Schweizer developed a line of gliders starting in World War II. The 1-30 was not intended to be a motor glider, but rather a light aircraft with some utilizing glider and sailplane technologies, common parts with other Schweizer designs, and an affordable price as a result of using smaller powerplants. Removable wings, and the ability to be transported by trailer were also criteria for keeping airport-based hangar costs down. The 1-30 shares the same wings and tail surfaces as the 1-26 glider. The fuselage is of aluminum construction with a welded steel tube tail structure. The wings are removable using the same design as the 1-26. The engine uses a cowling with exposed cylinders like a J-3 Cub for simplicity and cooling efficiency. Wing mounted spoilers were retained from the 1-26, allowing steep low-speed descents at about a 5:1 glide ratio. Three sets of wings were tested including a set from a model 2-31.
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