Sud-Ouest Djinn - Design and Development

Design and Development

Experience with the earlier Ariel experimental tip jet helicopter led Sud-Ouest to develop a practical light helicopter, the S.O.1221 Djinn. It did not use the same tip jet system but relied on compressed air being fed to the ends of the rotor blades. Apart from its method of propulsion the Djinn was a conventional helicopter with a two-seat side-by-side cabin and a Turbomeca Palouste turbo-compressor behind. The aircraft had an uncovered tail-boom with twin fins and a rudder. Because of the non-torque rotor propulsion it did not need an anti-torque tail rotor.

A single seat prototype (designated S.O.1220) tested the power conceptand first flew on 2 January 1953. This was a simple uncovered structure with an exposed seat for the pilot. This proved the viability of the propulsion system and five two-seat prototypes were then built as the S.O.1221, the first flew on 16 December 1953. Within a few days the helicopter had climbed to an altitude of 4,789 m (15,712 ft) to establish a record in its class.

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