Method of forming a composite structure such as a rocket combust

Details Method of forming a composite structure such as a rocket combust Method of forming a composite structure such as a rocket combust

1995-06-07

1999-01-05

Johnstone, Adrienne C.

Plastic and nonmetallic article shaping or treating: processes

Carbonizing to form article

2989001, 60253, 164 46, 164122, 164125, 228120, 264 295, 264 297, 264 81, 264162, 264219, 264317, 427228, 427250, 427251, B22D 2300, B05D 502, B05D 700, F02K 900

Patent

active

058558284

ABSTRACT:
A refractory composite structure is formed which comprises a ductile refractory metallic layer with a roughened surface which is tightly bonded to a refractory composite structural shell. The roughened surface is preferably dendritic in form and produced by chemical vapor deposition techniques. The refractory composite structural shell is preferably a carbon-carbon composite formed by applying a carbon filament preform to the roughened surface, infiltrating the preform with a carbon matrix precursor, and carbonizing the precursor.

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