Leduc 022

· René Leduc

Airplanes

Length

18.21 m

Flat Wing Span

9.95 m

Flat Wing Area

21.1 m²

Max Speed

1200 km/h

Max Mach

1.15 Mach

Max Ceiling

8800 m

Number of Engines

First Flight

1956-12-26

Number Built

Maximum Take-Off Weight

8.975 t (paragliders: kg)

Total Fuel Capacity

2728

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
Leduc 022	8.975	2728

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Mikoyan-Gurevich I-350		16.652	9.73	Compare
Shenyang J-13		17.5	10.4	Compare
McDonnell F3H Demon		17.9832	10.668	Compare
Chengdu J-10		16.9	9.8	Compare
Lavochkin La-190		16.35	9.9	Compare
Dassault Mirage IIIV	Pratt & Whitney / SNECMA TF104	18	8.72	Compare

All data (17 fields)

Name: Leduc 022
Manufacturer: René Leduc
Description: The Leduc 022 was the prototype of a mixed-power French interceptor built in the mid-1950s.
First Flight: 1956-12-26
Designer: René Leduc
Length (m): 18.21
Cockpit Crew: 1
Max Speed (km/h): 1200
Max Ceiling (m): 8800
Max Mach (Mach): 1.15
National Origin: France
Number Built: 2
Powerplant Description: 1 × Leduc ramjet, 63.6 kN thrust each
Wikipedia Article (URL): en.wikipedia.org/wiki/Leduc_022
Flat Wing Span (m): 9.95
Flat Wing Area (m²): 21.1
Number of Engines: 1