发明名称 Hybrid-type gas generator - for rocket motors
摘要 <p>Gas generator with a series of charges of solid fuel partic. in the form of a hollow burner, at least the front charge of which reacts with a liq. hyper gel oxidant applied to this charge only for the production initially of oxygen-rich gases and/or vapours which flow over the remaining solid fuel and progressively remove it by stoichiometric reaction, the special characteristic of this arrangement being that at least the front fuel charge has, apart from its ignitability by the oxidant, a relatively higher mechanical strength than the succeeding fuel charges with respect to the dynamic flow effects of the oxidant.</p>
申请公布号 DE2104498(A1) 申请公布日期 1972.08.10
申请号 DE19712104498 申请日期 1971.02.01
申请人 发明人
分类号 C06D5/10 主分类号 C06D5/10
代理机构 代理人
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