Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme
Vehicle

SNCASO SO.1221 Djinn

Lighter-Than-Air Craft and Rotorcraft

The Sud-Ouest SO.1221 Djinn was a French two-seat light helicopter, designed and built by SNCASO, which later merged into Sud Aviation. It was the first production French helicopter and the first production rotorcraft to use tip-jet propulsion: a Turbomeca Palouste gas turbine drove a pump that fed compressed air to the tips of the hollow rotor blades, so no anti-torque tail rotor was needed and directional control came from deflecting the engine exhaust. A single-seat test machine, the SO.1220, flew on 2 January 1953, and the first two-seat SO.1221 flew on 16 December 1953. The French Army ordered 100 helicopters, the German Army bought six, and ten further countries ordered the type, including for liaison, observation, training, casualty evacuation and crop spraying. Production ended in the mid-1960s after 178 had been built, as the more conventional Alouette II and Alouette III took over.

Facts
Year
1953 1
Engine Class
Gas turbine 1
Status
Out of production 1
Units Built
178 1
Top Speed (km/h)
130 1
Mass (kg)
360 1
Maximum Mass (kg)
800 1
Comparison
Body Style
Helicopter 1
Connections

Exemplifies

Source SNCASO SO.1221 Djinn (Wikipedia)

Of Make

Source SNCASO SO.1221 Djinn (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source SNCASO SO.1221 Djinn (Wikipedia)Development, Super Djinn
Quote, Development, Super Djinn
tentatively designated as the Djinn III or Super Djinn, was being studied by Sud Aviation

Originated In

Also in Geography Atlas: where this subject originated.

Source SNCASO SO.1221 Djinn (Wikipedia)Lead
Quote, Lead
is a French two-seat light helicopter
Sources
1. SNCASO SO.1221 Djinn (Wikipedia)
  • Development, first flight
    the first of these flew on 16 December 1953
  • Operational history
    a total of 178 Djinns had been constructed
  • Lead
    is a French two-seat light helicopter
  • Design
    a Turbomeca Palouste gas turbine engine that drove a pump to produce compressed air
  • Specifications, empty weight
    Empty weight: 360 kg (794 lb)
  • Specifications, gross weight
    Gross weight: 800 kg (1,764 lb)
  • Specifications, performance
    Maximum speed: 130 km/h (81 mph, 70 kn)
  • Operational history, status
    Production of the Djinn came to an end during the mid-1960s
  • Of Make: Sud Aviation, Development, Super Djinn
    tentatively designated as the Djinn III or Super Djinn, was being studied by Sud Aviation
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.