•
S.O. 4050-01 : Two-seat all-weather fighter prototype, powered by two 23.5-kN (5,291-lb) Atar 101B turbojet engines. First flew on 16 October 1952. One built. •
S.O. 4050-02 : Single-seat ground-attack prototype, powered by two 27.6-kN (6,217-lb) Atar 101D turbojet engines. First flew on 16 December 1953. One built. •
S.O. 4050-03 : Two-seat bomber prototype, powered by two
Armstrong Siddeley Sapphire turbojet engines. First flew on 5 December 1954. One built. The Vautour was produced in three principal variants, which had 90% commonality: •
IIA: Single-seat, long-range
attack aircraft, armed with cannon and bombs (carried internally or on four underwing pylons) •
IIN: Two-seat, all-weather interceptor with or
radar in nose, pilot and co-pilot in tandem seats, armed with cannon,
air-to-air missiles, and (theoretically) unguided rockets. The designation was later changed to
II-1N. •
IIB: Two-seat
bomber with glazed nose position for bombardier/observer replacing cannon pack, carrying bombs internally and on underwing pylons. Some IIB aircraft were converted to various specialized roles, principally
reconnaissance (
IIBR and
IIBN),
electronic countermeasures, and eventually target tug (
IIB-TT).
Production Total production was 149 aircraft, divided as follows: •
Prototypes: 3 •
Pre-production: 6 •
IIA: 30 (13 for France, 17 for Israel) •
IIB: 40 (36 for France, 4 for Israel) •
IIN: 70 (63 for France, 7 for Israel) ==Operators==