{
  "$type": "site.standard.document",
  "description": "Provided are an igniter-integrated thrust chamber for a rocket engine using a cryogenic fuel and liquid oxygen and a rocket including the thrust chamber. The thrust chamber includes a combustion chamber and a mixing head assembly, which is disposed at one side of the combustion chamber and is…",
  "path": "/patents/1315739",
  "publishedAt": "2022-04-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K9/95",
    "KOREA AEROSPACE RESEARCH INSTITUTE"
  ],
  "textContent": "Provided are an igniter-integrated thrust chamber for a rocket engine using a cryogenic fuel and liquid oxygen and a rocket including the thrust chamber. The thrust chamber includes a combustion chamber and a mixing head assembly, which is disposed at one side of the combustion chamber and is integrated with the combustion chamber.",
  "title": "THRUST CHAMBER INTEGRATED WITH IGNITER OF ROCKET ENGINE USING CRYOGENIC FUEL AND LIQUID OXYGEN AND ROCKET INCLUDING THE SAME"
}