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SPECIFICATIONS
  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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