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Aircraft H.M. 14 Pou Du Ciel

Aircraft H.M. 14 Pou Du Ciel © Konstantinos Panitsidis
Photo archive K. Panitsidi

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Prewar design by French engineer pilot Henri Mignet, who envisioned an aircraft that anyone could manufacture with simple houses materials of this aircraft was donated by the construction and owner Mr. Costas Karpathopoulo 1997 in aviation Greece academy, which in turn donated the Museum / HAF.

 


Technical specifications

DESIGNER Henri Mignet
COUNTRY France
TYPE
Ultralight aircraft
CREW 1
POWER-PLANT One Rotax 377 engine
Power, h.p. 1x35
DIMENSIONS
 
Length, m
4,40
Height, m
1,65
Wing span, m
6,00
Wing span tail unit, m 4,00
Wing area m2 -
WEIGHT  
Maximum take-off, kg 165
Normal take-off, kg -
Empty aircraft, kg -
Internal fuel, lt -
Payload, kg -
PERFORMANCE  
Maximum speed, km/h -
Cruising speed, km/h 85
Combat range, km
-
Range, km -
Ferry range, km -
Service ceiling, m -
Rate of climb, m/min -
Maximum overload, g -
ARMAMENT Doesn't have (defensive).





Photos H.M.14 Pou Du Ciel Ultralight aircraft