Maupin Woodstock ![]()
Woodstock was designed with a wing having an 18 % section for the root, 13 % at the tip and no twis. The principal design objectives were low cost and simplicity of construction. Douglas Air was used for all major structural parts and all tail and wing skins were birch. It first flew in 1978 and won the Sailplane Homebuilders Association design contest in 1984. A tail wheel is an option instead of a skid. The main wheel is fixed. Approach control is by wing top surface spoilers. As an option, wings of 13.1 m./ 43.0 ft. Woodstock
Wing span: 11.89 m / 41.5 ft
Wing area: 9.73 sq.m / 104.7 sq.ft
Aspect ratio: 14.5
Airfoil: Culver
Length 5.43 m / 17 ft 10 in
Height: 1.22 m / 4ft 0 in
Empty Weight: 111 kg / 245 lb
Payload: 95 kg / 210 lb
Gross Weight: 206 kg / 455 lb
Water ballast: None
Wing Load: 20.9 kg/sq.m / 4.29 lb/sq.ft
L/DMax: 24 at 72 kph / 39 kt / 45 mph
MinSink: 0.79 m/s / 2.6 fps / 1.54 kt
Seats: 1
Woodstock 15M
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