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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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