Nord Aviation CT20

· Nord Aviation

Airplanes

Length

5.45 m

Flat Wing Span

3.16 m

Flat Wing Area

3.2 m²

Max Speed

900 km/h

Max Mach

0.85 Mach

Max Ceiling

12000 m

Number of Engines

Entry Into service

1957-01-01

Maximum Take-Off Weight

0.66 t (paragliders: kg)

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Nord Aviation CT20	0.66

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
McDonnell Douglas X-36	Williams F112	5.4864	3.048	Compare
BQM-145 Peregrine	Teledyne CAE F408	5.6	3.2	Compare
NAMU KDN Gorgon	Westinghouse J32	4.8768	3.048	Compare
Moskalyev SAM-9 Strela	Renault 6P	6.15	3.55	Compare

All data (16 fields)

Name: Nord Aviation CT20
Manufacturer: Nord Aviation
Description: The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957.
Entry Into service: 1957-01-01
Designer: Nord Aviation
Length (m): 5.45
Cockpit Crew: 0
Max Speed (km/h): 900
Max Ceiling (m): 12000
Endurance (h): 55
Max Mach (Mach): 0.85
Powerplant Description: 1 × Turbomeca Marboré II turbojet, 3.92 kN thrust each
Wikipedia Article (URL): en.wikipedia.org/wiki/Nord_Aviation_CT20
Flat Wing Span (m): 3.16
Flat Wing Area (m²): 3.2
Number of Engines: 1