发明名称 Raketenmotoren mit Feststofftreibmitteln
摘要 1,040,662. Turbines. OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES. March 3, 1964 [March 5, 1963], No. 8987/64. Heading FIT. [Also in Division F3] A solid propellant which may be used to drive a turbine comprises two hemi-spherical blocks in contact over their plane surfaces E, each block consisting of at least two portions 1, 2, the portion 1, which is a sector of a sphere, being of faster burning powder than the portion 2. The casing 3 housing the propellant has two oppositely directed nozzles 4 to provide a torque.
申请公布号 DE1426416(A1) 申请公布日期 1969.01.30
申请号 DE19641426416 申请日期 1964.03.05
申请人 OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES DIT O.N.E.R.A. 发明人 LARUE,PIERRE
分类号 F02K9/12 主分类号 F02K9/12
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