Sud Aviation Vautour

· SNCASO

Airplanes

Length

15.57 m

Flat Wing Span

15.1 m

Height

4.94 m

Flat Wing Area

45 m²

Max Speed

1106 km/h

Max Mach

0.9 Mach

Max Ceiling

15200 m

Number of Engines

First Flight

1952-10-16

Entry Into service

1956-01-01

Maximum Take-Off Weight

21 t (paragliders: kg)

Maximum Range

5400 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Sud Aviation Vautour	21	5400

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
De Havilland Sea Vixen		16.764	15.5448	Compare
Sukhoi Su-25	Tumansky R-13	15.53	14.36	Compare
Fairchild Republic A-10 Thunderbolt II	General Electric TF34	16.26	17.53	Compare
Gloster Javelin		17.0688	15.8496	Compare
Sukhoi Su-28	Tumansky R-13	15.36	14.36	Compare
Northrop Tacit Blue		16.764	14.6304	Compare

All data (22 fields)

Name: Sud Aviation Vautour
Manufacturer: SNCASO
Description: The Sud-Ouest Aviation (SNCASO) S.O. 4050 Vautour (French for vulture) is a French jet-powered multirole aircraft.
First Flight: 1952-10-16
Entry Into service: 1956-01-01
Service End: 1979-01-01
Designer: SNCASO
Type: multirole aircraft
Length (m): 15.57
Height (m): 4.94
Cockpit Crew: 1
Max Speed (km/h): 1106
Max Ceiling (m): 15200
Rate of Climb (m/s): 60
Armament: 4 × 30 mm DEFA cannon, 100 rounds per gun; Internal weapons bay: Maximum of 2,725 kg (6,000 lb) of bombs (typically six 450 kg (1,000 lb) bombs), pack of 116 × 68 mm (2.7 in) rockets, camera pack, or two 1,500 liter (400 U.S. gal) fuel tanks; Four underwing pylons each rated at 1,500 kg (3,300 lb) inboard and 500 kg (1,100 lb) outboard
Max Mach (Mach): 0.9
Powerplant Description: 2 × SNECMA Atar 101E-3 turbojet engines, 34.3 kN thrust each
Primary Users: French Air Force, Israeli Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Sud_Aviation_Vautour
Flat Wing Span (m): 15.1
Flat Wing Area (m²): 45
Number of Engines: 2