{
  "$type": "site.standard.document",
  "description": "The motor (1) has a priming unit (8) arranged in a detonation chamber (3) for initiating detonation mixture. The detonation chamber is provided with an injection base (10), where length of the base is defined along an open line (17) to form the detonation chamber having elongated shape in a…",
  "path": "/patents/995854",
  "publishedAt": "2012-11-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K7/08",
    "MBDA FRANCE [FR]"
  ],
  "textContent": "The motor (1) has a priming unit (8) arranged in a detonation chamber (3) for initiating detonation mixture. The detonation chamber is provided with an injection base (10), where length of the base is defined along an open line (17) to form the detonation chamber having elongated shape in a transverse plane. An injection system (4) injects fuel/oxidant detonation mixture into the detonation chamber at the level of a segment of the base. A cooling circuit extends along a side wall of the detonation chamber.",
  "title": "Continuous detonation wave engine and aircraft provided with such an engine"
}