Guillemin JG.10

· Jean Guillemin · 1 × Renault 4P

Airplanes

Length

7.1 m

Flat Wing Span

13 m

Height

2.2 m

Flat Wing Area

23 m²

Max Speed

160 km/h

Max Ceiling

4500 m

Number of Engines

Aircraft Engine

First Flight

1931-06-01

Number Built

Total Fuel Capacity

130

Maximum Range

500 km

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity	Maximum Range (km)
Guillemin JG.10	130	500

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
AEG C.IV	Mercedes D.III	7.15	13.46		Compare
Dewoitine D.9	Bristol Jupiter	7.3	12.8		Compare
AMF Chevvron 2-32	König SD 570	7.01	13.41		Compare
De Bruyne Snark	De Havilland Gipsy Major	7.3152	12.8016	3	Compare
AEG J.I	Benz Bz.IV	7.2	13.46		Compare
Aviatik B.II (Germany)	Mercedes D.II	7.1	12.35		Compare

All data (17 fields)

Name: Guillemin JG.10
Manufacturer: Jean Guillemin
Description: The Guillemin JG.10 or Blériot-Guillemin JG.10 was a French two seat touring aircraft, designed to be as simple and safe to fly and maintain as a car, with similar facilities, as well as provision for parachutes.
First Flight: 1931-06-01
Designer: J. Guillemin
Length (m): 7.1
Height (m): 2.2
Max Speed (km/h): 160
Max Ceiling (m): 4500
National Origin: France
Number Built: 1
Powerplant Description: 1 × Renault 4Pb air-cooled 4-cylinder inline, 71 kW (95 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Guillemin_JG.10
Flat Wing Span (m): 13
Flat Wing Area (m²): 23
Aircraft Engine: Renault 4P
Number of Engines: 1