IP Library Granted Patent US 9,359,974
Granted Patent B2
US 9,359,974 · App. 14/224,214 · Granted Jun 7, 2016

High performance liquid rocket propellant

Inventor: Indresh Mathur (Sugar Land, TX)
Assignee: Johann Haltermann Limited
F02K9/42C06B25/20C10G35/095C10L1/04C10G2300/301C10G2400/08
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Quick Facts
Patent No.
US 9,359,974
App. No.
14/224,214
Granted
Jun 7, 2016
Kind
B2
Abstract

Disclosed is a process of fueling a rocket engine or air-breathing engine for a hypersonic vehicle with 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 C 12 -C 20 isoparaffin content of at least 40% by mass.

Claims (11)

1. A process of fueling a rocket engine or an air breathing engine of a hypersonic vehicle comprising:

introducing to the engine a hydrocarbon fuel 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 refined kerosene.

2. The process of claim 1 , in which the hydrocarbon fuel has a range of components that provide a boiling point range of at least 100° F.

3. The process of claim 1 , in which the hydrocarbon fuel has a net heat of combustion greater than 18.7 KBtu/lb.

4. The process of claim 1 in which the kerosene is a highly paraffinic refined kerosene.

5. The: process of claim 1 , in which the isoparaffin is comprised of at least one isododecane, at least one isohexadecane, at least one isoeicosane, or a mixture of these.

6. A process of fueling a rocket engine or an air breathing engine of a hypersonic vehicle comprising:

introducing to the engine 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, and wherein the hydrocarbon fuel is a blend of an isopareffin and a refined kerosene.

7. The process of claim 6 , in which the hydrocarbon fuel has a net heat of combustion greater than 18.7 KBtu/lb.

8. The process of claim 6 , in which the kerosene is a highly paraffinic refined kerosene.

9. The process of claim 6 , in which the isoparaffin is comprised of at least one isododecane, at least one isohexadecane, at least one isoeicosane, or a mixture of these.

Assignments (2)
CHANGE OF NAME Recorded Dec 5, 2018
From: JOHANN HALTERMANN LTD
To: MONUMENT CHEMICAL HOUSTON, LTD
Reel/Frame 047728/0913 →
ENTITY CONVERSION Recorded Dec 5, 2018
From: MONUMENT CHEMICAL HOUSTON, LTD
To: MONUMENT CHEMICAL HOUSTON, LLC
Reel/Frame 047728/0959 →
Continuity (3)
Division 13670776 · Nov 7, 2012
Provisional Application 61615088 · Mar 23, 2012
Related Publication 20140202132A1 · Jul 24, 2014