{
  "$type": "site.standard.document",
  "description": "A missile comprises a propulsion system, a passageway (1) for delivering air to the propulsion system and a ducting element (9) associated with the passageway (1). The ducting element (9) has a ducting surface for ducting air into the passageway (1), and the ducting element (9) is rotatable, about…",
  "path": "/patents/1001649",
  "publishedAt": "2012-06-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "MBDA UK LTD [GB]"
  ],
  "textContent": "A missile comprises a propulsion system, a passageway (1) for delivering air to the propulsion system and a ducting element (9) associated with the passageway (1). The ducting element (9) has a ducting surface for ducting air into the passageway (1), and the ducting element (9) is rotatable, about an axis (13) that is aligned, or more preferably co-axial, with the axis (19) of the passageway (1), from a stowed position in which the ducting surface is received in the passageway (1), to a deployed position in which the ducting surface protrudes from the passageway (1) to duct air into the passageway.",
  "title": "An air intake system for an air vehicle"
}