High performance liquid rocket propellant
AssigneeJohann Haltermann Limited
InventorIndresh Mathur
Life of this patent
Estimating the term…
Abstract
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.
Claims22
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.
A hydrocarbon fuel having a range of components that provide a boiling point range of at least 100° F., and having a hydrogen to carbon ratio greater than 2.0 on an atomic basis.
(canceled)
(canceled)
A fuel composition comprising:
- a total paraffin content of at least 90% by mass;
- and
- wherein the composition contains at least 40% by mass of isoparaffins having from 12 to 20 carbon atoms.
Dependencies are inferred from the claim text.