发明名称 |
Low viscosity air breathing missile fuel |
摘要 |
An improved ramjet fuel consisting of hydrogenated hydrocarbons uses a minimum weight percentage of 50% tetrahydromethylcyclopentadiene dimer (TH-dimer) with about 50% by wt. exo-tetrahydrodicyclopentadiene (Exo-THDC). The mixture exceeds U.S. Navy flash point requirements of 60 DEG C. while yielding a lower viscosity than TH-dimer alone. Volumetric heating properties of the mixture make it an excellent ramjet fuel.
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申请公布号 |
US4427467(A) |
申请公布日期 |
1984.01.24 |
申请号 |
US19820373080 |
申请日期 |
1982.04.29 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY |
发明人 |
BURDETTE, GEORGE W.;HALL, LEWIS |
分类号 |
C10L1/04;F02K9/42;(IPC1-7):D03D23/00 |
主分类号 |
C10L1/04 |
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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