: : US Pacific - Home of the Mitchell Wing Ultralights : :

	B-10	U-2
MECHANICAL
Engine Requirements:	15-40 hp	25-50 hp
External Dimensions: Wing Span Wing Area Length Overall Height Overall	34 ft. 136 sq. ft. 8 ft. 4 ft.	34 ft. 136 sq. ft. 9 ft. 4.5 ft.
Weight and Loadings: Pay Load Empty Weight Seats Wing loading	350 pounds 245 pounds 1 person +/- 4 g	350 pounds 320 pounds 1 person +/- 4 g
Materials:	Composite	Wood and Fabric
Control:	Conventional 3-Axis	Conventional 3-Axis
Aspect Ratio:	8:1	8:1
Propeller:	Fixed Pitch, wooden (50 X 25 or 50 X 27)	Fixed Pitch, wooden (50 X 23 or 50 X 30)
Airfoil:	Modified NACA 23015	Modified Wortman
PERFORMANCE
Cruise Speed:	35-60 mph	40-75 mph
Max. Cruise(sea level):	65 mph	95 mph
Fuel Consumption:	1-1.5 gph	1.2-2 gph
Glide Ratio:	16:1	22:1
Rate of Climb:	600 fpm (w/Zenoah 250 engine)	600 fpm ( w/Zenoah 250 engine)
Service Ceiling:	12,000 ft.	12,000 ft.
Stall Speed:	25 mph	34 mph
Takeoff Ground Roll:	200 ft.	250 ft.
Landing Ground Roll :	150 ft.	250 ft.
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