SNCASO SO.9000 Trident

Sud-Ouest (SNCASO) · France · first flew 1953 · fighter

The SNCASO SO.9000 Trident was a French experimental mixed-power interceptor that combined wingtip-mounted Viper turbojets with a central rocket motor for high-speed dash capability. It achieved Mach 1.6 in tests but the programme was not developed to production.

Recognition (WEFT)

W — WingsMid-mounted, delta
E — Engines2 × rocket, wing-mounted
F — FuselageVery narrow fuselage and delta wing design
T — TailNo tailplane

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Spot it by:

Immediately distinguished by turbojets mounted in pods at the wingtips, a slender fuselage with a central rocket exhausted at the tail, and pure delta planform with no tail surfaces.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Developed in the early 1950s as France explored various approaches to high-performance interception, the Trident used the novel layout of turbojets at the wingtips (for take-off and cruise) combined with a central liquid-fuel rocket for high-altitude dash. The aircraft was extremely fast for its era but the complex mixed propulsion system was impractical for service, and it was cancelled in favour of the more conventional Mirage series.

Variants

Three prototypes in the SO.9000 series were built with progressive changes; the SO.9050 Trident II was a refined follow-on.

Where you'll see it

Never entered operational service; all aircraft were test vehicles expended in the flight development programme.

Related aircraft

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