Technical Doc Number 8456. Notice Pilote dated 1955, 47 pages
details ,schematic drawings, check lists,systems,electrics,fuselage , fuel, instruments , charts , wiring electrical, reactures, hydraulics, etc. French Language pages samples as shown
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historic aviation data preserved forever , rare factory manual for this Experimental Jet
Fascinating material easy use on any computer, view enlarge , print the documents in full or individual images/pages. Colour cast and blue white pages , see samples .
AS ONCE USED WITH THESE FAMOUS JETS
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The SNCASO SO.9000 Trident was a French mixed-power interceptor aircraft developed and constructed by aircraft manufacturer SNCASO. While having achieving promising results during testing, including the establishment of several world records during flight tests, the French Government chose to cancel its order for the Trident, leaving it as a development programme only. This was perhaps atributed to the British Defence white paper . This saw a large number of advanced aircraft development programmes ( inc mixed-power interceptors) abruptly aborted in favour of development of missiles.
Variants
SO.9000 Trident I
Two aircraft built: the first aircraft, 01, was built at Istres and was completed in late 1952, the second aircraft, 02, crashed on its first flight on 1 September 1953. Powered by two 3.924 kN (882 lbf) Turbomeca Marboré II turbojet engines with a single three-chamber SEPR 481 rocket engine, each chamber producing 12.25 kN (2,755 lbf) thrust.
SO.9050 Trident II
Three prototype and ten pre-series aircraft ordered in 1953 and first flown on 21 December 1955: Pre-series aircraft were powered by two 10.79 kN (2,430 lbf) Turbomeca Gabizo with a two-chamber (13 kN (3,000 lbf) per chamber) SEPR 631 rocket engine (each chamber now being individually ignited for finer thrust control). SO.9050 prototypes 001, 002 and 003 were powered by two 2x 7.31 kN (1,640 lbf) Dassault MD.30 Viper turbojet, and SEPR 631 rocket engines.
SO.9050 Trident III
SO.9050-07, -08 and -09, powered by two 14.71 kN (3,310 lbf) Turbomeca Gabizo turbojets with a SEPR 631 rocket engine.
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