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 US9005380(B2) 申请公布日期 2015.04.14
申请号 US201213670776 申请日期 2012.11.07
申请人 Johann Haltermann Limited 发明人 Mathur Indresh
分类号 C10G35/095;C06B25/20;F02K9/42;C10L1/04 主分类号 C10G35/095
代理机构 Butzel Long 代理人 Butzel Long
主权项 1. A hydrocarbon fuel having a range of components that provide a boiling point range of at least 100° F., and having a hydrogen content greater than 14.3% on a mass basis, an aromatics content of less than 5% by volume, a sulfur content of less than 30 ppm by mass, and wherein the hydrocarbon fuel is a blend of an isoparaffin and a kerosene.
地址 Houston TX US