A rocket engine nozzle that is steerable by means of a moving diverging portion on,申请号IL20030162928-传众专利搜索

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发明名称	A rocket engine nozzle that is steerable by means of a moving diverging portion on
摘要
申请公布号	IL162928(D0)	申请公布日期	2005.11.20
申请号	IL20030162928	申请日期	2003.07.03
申请人	SNECMA PROPULSION SOLIDE	发明人
分类号	F02K1/00;F02K9/84;(IPC1-7):F02K	主分类号	F02K1/00
代理机构		代理人
主权项
地址

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