{
  "$type": "site.standard.document",
  "description": "The system has an accessory sample (11) produced from a fuel-lot in addition to a rocket. The sample includes an engine combustion chamber, which is filled with a solid-propellant from the fuel-lot and corresponds to an engine combustion chamber of the rocket that is filled with the propellant. The…",
  "path": "/patents/985067",
  "publishedAt": "2013-04-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K9/00",
    "BAYERN CHEMIE GMBH FLUGCHEMIE [DE]"
  ],
  "textContent": "The system has an accessory sample (11) produced from a fuel-lot in addition to a rocket. The sample includes an engine combustion chamber, which is filled with a solid-propellant from the fuel-lot and corresponds to an engine combustion chamber of the rocket that is filled with the propellant. The propellants of the sample and the rocket adhere at a combustion chamber wall. The propellant of the sample is provided with dual stress and temperature sensors (12-15) at a surface, which adheres at the wall. The sensors are coupled with a data detecting device (16) of the sample.",
  "title": "SYSTEM FOR LIFESPAN MONITORING OF MISSILES"
}