{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "The solid propellant (12) has a burning chamber (16) withy one partition (26a) and another partition (26b) that are separated from each other by a partition wall (24). Former partition has a propellant (28a), which is arranged to be ignited in latter partition independent from another propellant…",
  "path": "/patents/980156",
  "publishedAt": "2014-01-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K9/12",
    "MBDA DEUTSCHLAND GMBH [DE]"
  ],
  "textContent": "The solid propellant (12) has a burning chamber (16) withy one partition (26a) and another partition (26b) that are separated from each other by a partition wall (24). Former partition has a propellant (28a), which is arranged to be ignited in latter partition independent from another propellant (28b). The partition wall has a plate stretching in longitudinal direction (L). The plate is connected at edges with an outer wall (20) of the burning chamber, so that the partitions are formed in wedge-shape or cylindrical segment shape. Independent claims are included for the following: (1) a method for operating a solid propellant; and (2) a missile.",
  "title": "Solid-fuel propulsion device"
}