Nord 1500 Griffon

Length
14.54 m
Flat Wing Span
8.1 m
Height
5 m
Flat Wing Area
32 m²
Max Speed
2320 km/h
Max Mach
2.19 Mach
Number of Engines
1
Aircraft Engine
First Flight
1955-09-20
Number Built
2
Maximum Take-Off Weight
6.745 t (paragliders: kg)

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
Nord 1500 Griffon 6.745

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All data (21 fields)
Name
Nord 1500 Griffon
Manufacturer
Nord Aviation
Description
The Nord 1500 Griffon is an experimental ramjet-powered interceptor aircraft designed and built by French state-owned aircraft manufacturer Nord Aviation.
First Flight
1955-09-20
Service End
1961-01-01
Designer
Nord Aviation
Type
Experimental interceptor
Length (m)
14.54
Height (m)
5
Cockpit Crew
1
Max Speed (km/h)
2320
Rate of Climb (m/s)
86.67
Max Mach (Mach)
2.19
National Origin
France
Number Built
2
Powerplant Description
1 × SNECMA Atar 101E-3 turbojet engine, 34.3 kN thrust each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Nord_1500_Griffon
Flat Wing Span (m)
8.1
Flat Wing Area (m²)
32
Aircraft Engine
SNECMA Atar 101
Number of Engines
1