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METHODS OF FORMING FLEXIBLE STRUCTURES FOR A ROCKET MOTOR ASSEMBLY, RELATED FLEXIBLE STRUCTURES, AND RELATED ASSEMBLIES INCLUDING THE FLEXIBLE STRUCTURES
METHODS OF FORMING FLEXIBLE STRUCTURES FOR A ROCKET MOTOR ASSEMBLY, RELATED FLEXIBLE STRUCTURES, AND RELATED ASSEMBLIES INCLUDING THE FLEXIBLE STRUCTURES
A method of forming a flexible structure for a rocket motor assembly comprises forming a polysiloxane composition comprising at least two different silicone materials. A preliminary structure is formed from the polysiloxane composition. The preliminary structure is cured to crosslink at least a portion of different polysiloxane chains of the preliminary structure. A flexible structure for a rocket motor assembly, a flexible assembly for a rocket motor assembly, a moveable thrust nozzle assembly for a rocket motor assembly, and a rocket motor assembly are also described.
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