{
  "$type": "site.standard.document",
  "description": "Supply of a liquid fuel or comburent to a combustion chamber (2) of a rocket engine (1) is controlled by a feed valve (14) provided with an obturator (22) mobile between an open position and a closed position of at least one supply pipe (18), which has an inlet (21) that communicates with a tank…",
  "path": "/patents/1011417",
  "publishedAt": "2011-06-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K9/56",
    "SELEX GALILEO SPA [IT]"
  ],
  "textContent": "Supply of a liquid fuel or comburent to a combustion chamber (2) of a rocket engine (1) is controlled by a feed valve (14) provided with an obturator (22) mobile between an open position and a closed position of at least one supply pipe (18), which has an inlet (21) that communicates with a tank (13) for containing the liquid component and an outlet (17) that communicates with the combustion chamber (2); the displacement of the obturator (22) from its closed position to its open position being triggered by a pressurized fluid supplied to the outlet (17) of the supply pipe (18).",
  "title": "Rocket engine and method for controlling supply of fuel or comburent to the rocket engine"
}