Talk:Schreder HP-11

Info from article before major edits. Some of this can be moved to the new info box. --Brad101 02:51, 7 July 2006 (UTC)

Designed in USA by R.E. Schreder in 1962 L/D: 	  37:1 @ 54 mph, 86 km/h MinSink:  0.55 m/s (1.8 ft/s) @ 47 mph, 75 km/h Span 	       Area 	        Empty Weight 	Payload 	Gross Weight m 	ft 	m² 	ft² 	kg 	lb 	kg 	lb 	kg 	lb. 15.85 	52 	9.66 	104 	181 	400 	113 	250 	294 	650
 * 1) built 73+ all metal Gliders

Aspect ratio: 	26 Airfoil: 	NACA 65 (3)-618