发明名称 Combustion chamber used for a rocket propulsion system is made from a composite ceramic
摘要 Combustion chamber is made from a composite ceramic (e.g. metal, alloy, ceramic and/or carbon). Preferred Features: All segments of the drive mechanism, such as the main chamber, nozzle throat and expansion nozzle are made from the same composite structure. The chamber comprises a core (5), a separating layer (4), an inner shell (3), a casing (2) and an outer flange (1).
申请公布号 DE10106772(A1) 申请公布日期 2002.09.05
申请号 DE20011006772 申请日期 2001.02.09
申请人 MOK, HAU-PO 发明人 MOK, HAU-PO
分类号 F02K1/82;F02K9/62;F02K9/97;(IPC1-7):F02K9/62;F02K9/42 主分类号 F02K1/82
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