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.
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
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