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YF-130,即“500吨级液氧煤油发动机”,是中華人民共和國研制中的一型液體火箭發動機,该发动机基于YF-100的分级燃烧循环技术,采用双喷管设计,理论推力达到500吨级,是全世界目前推力最大的双燃烧室火箭发动机。该机计划将用於長征九號系列火箭的助推器及芯一級主发动机。目前首台工程样机已组装完成,等待进一步的改进测试。
, The YF-130 is a Chinese rocket engine fueled by LOX and kerosene in an oxidizer-rich staged combustion cycle currently in development. It has been designed to reach around 500 tonnes of thrust and it will power the super heavy Long March 9 rocket.
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rdfs:comment |
YF-130,即“500吨级液氧煤油发动机”,是中華人民共和國研制中的一型液體火箭發動機,该发动机基于YF-100的分级燃烧循环技术,采用双喷管设计,理论推力达到500吨级,是全世界目前推力最大的双燃烧室火箭发动机。该机计划将用於長征九號系列火箭的助推器及芯一級主发动机。目前首台工程样机已组装完成,等待进一步的改进测试。
, The YF-130 is a Chinese rocket engine fueled by LOX and kerosene in an oxidizer-rich staged combustion cycle currently in development. It has been designed to reach around 500 tonnes of thrust and it will power the super heavy Long March 9 rocket.
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rdfs:label |
YF-130
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