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Scanlan SG-1A
The Scanlan SG-1A is an American, single seat, pod-and-boom, high-wing, strut-braced glider that was designed by Thomas W. Scanlan in 1970 and sold in the form of plans for amateur construction.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 18. Soaring Society of America, November 1983. USPS 499-920〕
==Design and development==
The SG-1 was conceived as a very simple and economical aircraft that could be built with modest construction skills and very little financial investment. The prototype was completed in 1970 for US$400 and subsequent aircraft were built for under US$1000.〔〔
The SG-1 is constructed with a welded steel fuselage and tail surfaces and covered with doped aircraft fabric. The wing is made from an aluminium structure, covered in aluminum sheet and features upper-surface spoilers and a modified Gö 549 airfoil. The landing gear is a monowheel with the forward fuselage protected by a skid. The airframe was static tested to 9g without failing.〔〔
With a very low stall speed of , pilots who have flown the aircraft claim that the SG-1 can fly a thermal inside a Schweizer SGS 1-26.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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