Patent ID: 6890660
Filing Date: 2005-05-10
Classification: F23M,F23R,Y02T,Y10S,Y10T

Abstract:
1. A combustion chamber for a rocket drive, comprising: at least one first jacket made of a composite material with a ceramic matrix; and a load bearing external jacket that envelopes said at least one first jacket; wherein, said composite material comprises a fibrous structure made of carbon-containing fibers; and said fibrous structure comprises first, second and third layers of fiber bundles forming a three-dimensional matrix; fiber bundles of said first layer of fiber bundles extend in a first direction in space; fiber bundles of said second layer of fiber bundles extend in a second direction in space; fiber bundles of the third layer of fiber bundles extend in a third direction in space, said first, second and third directions being substantially divergent relative to each other; and the individual layers penetrate each other at least partially.