发明名称 SOLID PROPELLANT ROCKET MOTOR
摘要 A solid propellant rocket motor (1) has a tubular casing (3) accommodating a mass (5) of solid propellant material and at least one opening (10) for the space in the casing (3) to communicate with the outside closed by a closing head (11); the closing head (11) being coupled to the casing (3) by means of one or the other of two blocking portions (28) (21A) with different strength both carried by a movement device (21,35) which can be elastically deformed and operated from the outside.
申请公布号 WO2015151062(A1) 申请公布日期 2015.10.08
申请号 WO2015IB52448 申请日期 2015.04.02
申请人 AVIO S.P.A. 发明人 BELLOMI, PAOLO;MANCINI, VINCENZO
分类号 F02K9/26;F02K7/10;F02K9/10;F02K9/32;F02K9/34;F02K9/36;F02K9/38;F02K9/86 主分类号 F02K9/26
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