发明名称 |
System for lifespan monitoring of missiles |
摘要 |
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. |
申请公布号 |
EP2581594(A2) |
申请公布日期 |
2013.04.17 |
申请号 |
EP20120188116 |
申请日期 |
2012.10.11 |
申请人 |
BAYERN-CHEMIE GESELLSCHAFT FUER FLUGCHEMISCHE ANTRIEBE MBH |
发明人 |
TUSSIWAND, GIUSEPPE;MUSBACH, GUENTER;THUMANN, ALBERT;STEINFELD, HOLGER |
分类号 |
F02K9/00;F02K9/26 |
主分类号 |
F02K9/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|