{
  "$type": "site.standard.document",
  "description": "The multilayered composite material for combustion chambers or nozzles of flying craft comprises an inner layer consisting of fiber reinforced ceramics whose matrix contains phases of carbon and/or phases of silicon carbide. The outer layer of the material consists of a plastic material reinforced…",
  "path": "/patents/1090544",
  "publishedAt": "2004-01-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B29C70/088",
    "SGL CARBON AG [DE]"
  ],
  "textContent": "The multilayered composite material for combustion chambers or nozzles of flying craft comprises an inner layer consisting of fiber reinforced ceramics whose matrix contains phases of carbon and/or phases of silicon carbide. The outer layer of the material consists of a plastic material reinforced by carbon fibers. Independent claims are also included for: (a) a method for producing the proposed multilayered compound material; and (b) an application of the proposed compound material for construction of combustion chambers or nozzles of rockets.",
  "title": "Multi-layer sandwich material"
}