H.M. 14 POU DU CIEL. Ultralight aircraft © Konstantinos Panitsidis

Photos from the personal collection of Konstantinos Panitsidis


 Technical specifications      Photos      Video

 

 

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
1 x Rotax 377
Power h.p
1 x 35
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 -
PERFORMANCE  
Maximum speed, km/h -
Cruising speed, km/h
85
Service ceiling, m
-
Range, km
-
Combat range, km
-
Payload, kg -
ARMAMENT
-

 


PHOTOS H.M.14 Pou Du Ciel