Pyrotechnic ignition chain of a main propulsion charge of a missile.
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Exhaust system for gas turbine
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Cmc mixer with structural external coverage
FR2914707A1
Assembly method with recovery of two pieces having different expansion coefficients and assembly so obtained
FR2913718A1
Turbine ring assembly for gas turbine
FR2913717A1
Ring assembly for e.g. aircraft engine gas turbine, has centering unit constituted of metallic ring gear and bracket, and centering complete ring, where elastically deformable tab blocks rotation of ring around axis of ring
FR2912469A1
Method for manufacturing a lobe structure of cmc flux mixer for aeronautical gas turbine engine.
FR2910630A1
Thermo-erosive test device and method for thermal protective materials of solid propergol propellers
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Piece of ceramic matrix composite material containing silicon, protected against corrosion
FR2909920A1
Method for producing a carter-divergent assembly
FR2902803A1
Fibrous reinforcing structure for a piece of composite material and part comprising the same
FR2902802A1
Fibrous reinforcing structure for a piece of composite material and part comprising the same
FR2900420A1
Method for making fibrous strate for manufacturing a composite part preform
FR2899226A1
Piece of composite material with ceramic matrix containing silicon, protected against corrosion.
FR2893939A1
Oxidation protection of composite materials containing carbon
FR2892644A1
Trapping structure for fluid exchange column
FR2888211A1
Device and method for latch control for tuyere with rectangular output section
FR2886640A1
Method and preform for the production of composite material parts by cvi densification and pieces obtained
FR2885542A1
METHOD OF FORMING A SOLID DEPOSITION ON A SURFACE OF A SUBSTRATE OR WITHIN A POROUS SUBSTRATE
FR2882356A1
METHOD FOR MANUFACTURING PIECE OF COMPOSITE MATERIAL WITH CERAMIC MATRIX AND PART THUS OBTAINED
