<p>#CMT# #/CMT# The device has a primary ignition charge (4) and a solid propellant (6) arranged in the combustion chamber (1) of the rocket motor for igniting the gel propellant that is to be injected. The primary ignition charge has an ignition pill and a pyrotechnic transfer charge. #CMT#USE : #/CMT# For igniting a gel propellant for a rocket motor. #CMT#ADVANTAGE : #/CMT# Reliable, simple and of low mass. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic sectional representation of a combustion chamber of a rocket motor 1 : combustion chamber 3 : injection nozzle 4 : primary ignition charge 5 : combustion chamber wall 6 : solid propellant.</p>
申请公布号
EP2025908(B1)
申请公布日期
2015.01.21
申请号
EP20080010148
申请日期
2008.06.04
申请人
BAYERN-CHEMIE GESELLSCHAFT FÜR FLUGCHEMISCHE ANTRIEBE MBH
发明人
RAMSEL, JÜRGEN;STIERLE, RALF;NAUMANNL, KARL WIELAND