{
  "$type": "site.standard.document",
  "description": "The system (10) has a cylinder-shaped housing (11) comprising a retaining area (22) that is coupled with a pipeline of a fuel supply-line system (21). An elastic body (12) is arranged in the area and deformable by impact produced through flowing of fuel into the line system during opening of a tank…",
  "path": "/patents/1012217",
  "publishedAt": "2011-06-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64G1/402",
    "ASTRIUM GMBH [DE]"
  ],
  "textContent": "The system (10) has a cylinder-shaped housing (11) comprising a retaining area (22) that is coupled with a pipeline of a fuel supply-line system (21). An elastic body (12) is arranged in the area and deformable by impact produced through flowing of fuel into the line system during opening of a tank shut-off device of the line system in such a manner that the impact is damped, where the body is designed as a bellows. The elastic body is made from metal i.e. titanium, and a spring (13) is arranged in an inner side of the elastic body for adjusting spring rigidity of the attenuation system. An independent claim is also included for a spacecraft propulsion system comprising a power train and an attenuation system.",
  "title": "Attenuation element for a fuel supply line system of a spacecraft propulsion system"
}