Hurel-Dubois Miles HDM.105

· H.D. et M (Aviation) Ltd.
Airplanes
Length
10.3632 m
Flat Wing Span
22.86 m
Height
3.9624 m
Flat Wing Area
25.7341 m²
Flat Wing Aspect Ratio
20.5
Max Seating
9
Cruise Speed
186.6839 km/h
Max Speed
204.3867 km/h
Max Ceiling
4937.76 m
Number of Engines
2
First Flight
1957-03-31
Number Built
1
Total Fuel Capacity
120

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Aircraft Weight Variants

Aircraft Total Fuel Capacity
Hurel-Dubois Miles HDM.105 120

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All data (22 fields)
Name
Hurel-Dubois Miles HDM.105
Manufacturer
H.D. et M (Aviation) Ltd.
Description
The Hurel-Dubois Miles HDM.105 was a transport aircraft fitted with very high aspect ratio wings for research purposes, building on research carried out with the Hurel-Dubois HD.10, and a stepping point to the planned production HDM.106 Caravan.
First Flight
1957-03-31
Designer
Maurice Hurel
Length (m)
10.3632
Height (m)
3.9624
Cockpit Crew
2
Max Seating
9
Max Speed (km/h)
204.3867
Cruise Speed (km/h)
186.6839
Max Ceiling (m)
4937.76
Rate of Climb (m/s)
3.3376
Capacity Description
up to 9 passengers or freight
National Origin
France
Number Built
1
Powerplant Description
2 × Blackburn Cirrus Major III 4-cylinder inverted air-cooled in-line piston engines, 116 kW (155 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Hurel-Dubois_Miles_HDM.105
Flat Wing Span (m)
22.86
Flat Wing Area (m²)
25.7341
Flat Wing Aspect Ratio
20.5
Number of Engines
2