发明名称 HIGH PERFORMANCE LIQUID ROCKET PROPELLANT
摘要 Disclosed is a high performance hydrocarbon fuel characterized by a hydrogen content greater than 14.3% by weight, a hydrogen to carbon atomic ratio greater than 2.0 and/or a heat of combustion greater than 18.7 KBtu/lb. The disclosed fuels generally have a paraffin content that is at least 90% by mass and a C12-C20 isoparaffin content of at least 40% by mass.
申请公布号 WO2014011250(A4) 申请公布日期 2014.05.22
申请号 WO2013US33691 申请日期 2013.03.25
申请人 JOHANN HALTERMANN LIMITED;MATHUR, INDRESH 发明人 MATHUR, INDRESH
分类号 C10L1/04 主分类号 C10L1/04
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