SO 4050 Vautour

Summary

Category Combat Aircraft
Origin country 🇫🇷 France
ManufacturerSud Aviation
First flight16 October 1952
Year introduced1956
Number produced149 units
Average unit price$2 million

Description

In response to a 1951 French Air Force requirement for a multirole jet, the aircraft company SNCASO (later Sud Aviation) adapted its existing S.O. 4000 prototype. The resulting design, the S.O. 4050, performed its maiden flight on October 16, 1952, and demonstrated promising performance, even exceeding Mach 1 in a dive during early testing. Initial prototypes were tested with various British and French engines, but the production aircraft, named Vautour II, were powered by the indigenous SNECMA Atar turbojet. Though originally planned for a large production run, the Vautour was seen as a stop-gap, particularly in the strategic bomber role, and was maligned as obsolete and underpowered for much of its service life. Production ceased after 149 aircraft were manufactured, with the type entering service in 1958 and retiring in 1979 from French frontline units.

The Sud Aviation Vautour is a mid-sized, swept-wing monoplane featuring a 35-degree wing sweep, a "flying" tail, and two SNECMA Atar 101 turbojet engines mounted in pods beneath the wings. It utilizes a bicycle-type landing gear with main units under the fore and aft fuselage, stabilized by smaller outrigger gear in the engine pods. A significant portion of the fuselage is dedicated to a 5.0-meter internal weapons bay and fuel tanks. Key limitations, particularly in the Vautour IIB bomber variant, included the absence of radar and modern navigation systems, relying instead on a World War II-era Norden bombsight housed in a glazed nose section. The Vautour IIN interceptor variant, however, was equipped with radar for all-weather operations.

The Vautour could be configured with a variety of armaments to suit its multirole capability. A typical armament included four 30 mm DEFA cannons, each supplied with 100 rounds. The internal weapons bay could accommodate a maximum of 2,725 kg (6,000 lb) of munitions, including conventional bombs, a pack of 116 rockets, or a camera pack. Four underwing hardpoints allowed for an additional 4,000 kg of external stores, such as bombs, rockets, or napalm tanks. As a core component of France's early force de frappe, the Vautour IIB bomber was also capable of carrying a single AN-11 or AN-22 nuclear weapon in its internal bay.

The Vautour served with two operators: the French Air Force and the Israeli Air Force (IAF). In French service, it equipped bomber, all-weather fighter, and reconnaissance squadrons but never saw combat. Forty Vautour IIBs formed the initial airborne component of France's nuclear deterrent but were quickly supplemented and replaced by the Dassault Mirage IV due to the Vautour's perceived performance limitations. The IAF had a more active combat career with the type, employing it in attack, reconnaissance, and electronic warfare roles during the Six-Day War and the War of Attrition. Though it scored a single air-to-air kill against an Iraqi Hawker Hunter, it was more valued for its range and bombing capabilities. The IAF retired its last Vautours in 1972, replacing them with the Douglas A-4 Skyhawk.

Main Variants

  • IIA: A single-seat, long-range attack variant armed with cannons and capable of carrying bombs both internally and on underwing pylons.
  • IIN: A two-seat, all-weather interceptor equipped with a nose-mounted radar and crewed by a pilot and co-pilot in tandem seats.
  • IIB: A two-seat bomber version which replaced the cannon pack with a glazed nose for a bombardier/observer.
  • IIBR: A designation for Vautour IIB aircraft that were converted for specialized photo reconnaissance missions.

Technical specifications

Version: Vautour IIA
Crew1
Operational range5,400 km (3,355 mi)
Maximum speed 1106 km/h (687 mph)
Wing area45 m² (484.4 sqft)
Wingspan15.1 m (49.5 ft)
Height4.9 m (16.2 ft)
Length15.6 m (51.1 ft)
Service ceiling15,200 m (49,869 ft)
Empty weight10,000 kg (22,046 lbs)
Max. takeoff weight21,000 kg (46,297 lbs)
Climb rate60.0 m/s (196.9 ft/s)
Powerplant2 × SNECMA Atar 101E-3 turbojet engines
Ejection seatDassault E-101

Current operating countries

No country is operating the SO 4050 Vautour in 2025.

All operators

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