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 |