Miles Libellula (M.35) Aircraft
| |
Production Details | |
Design Company: |
Phillips & Powis Aircraft Ltd |
First Flight: |
1 May 1942 |
M.35 Libellula: |
1 - Phillips & Powis, Woodley |
Type Specification | |
Applies to: |
Miles M.35 Libellula |
Type: |
Experimental aircraft to Miles own specification |
Wing: |
Tandem wing design. Forward wing mounted on top of fuselage just aft of cockpit. Wing has straight leading edge and tapers towards the tip and is fitted with flaps and elevators. Rear wing is mounted at rear of fuselage with highly swept outer sections and is fitted with flaps and ailerons. |
Fuselage: |
Constant section wooden fuselage |
Tail Unit: |
No tail, fins and rudders mounted at tips of rear wing |
Landing Gear: |
Fixed tricycle. Nose wheel mounted under forward wing, main wheels mounted under rear wing |
Power Plant: |
One 130 hp de Havilland Gipsy Major engine driving pusher propeller in rear of fuselage |
Accommodation: |
Single seat for pilot in enclosed cockpit in nose |
Dimensions | |
Span: |
20 ft 5 in |
Length: |
Unknown |
Height: |
Unknown |
Wing Area: |
134 sq ft |
Weights | |
Empty: |
1,456 lb |
All-up: |
1,850 lb |
Performance | |
Max Speed: |
Unknown |
Preserved in British Museums | |
None known | |
Web Sites | |
http://www.jaapteeuwen.com/ww2aircraft/html%20pages/MILES%20M35.htm |