High volumetric energy density rocket propellant

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10065900
APP PUB NO 20170183273A1
SERIAL NO

15157935

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Abstract

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A rocket propellant includes a hydrocarbon blend having a total aromatic compounds content less than 0.5 mass percent, a specific energy of at least 18.4 KBtu/lb, and a mass density of at least 0.8150 grams per cubic centimeter. The propellant, which can be prepared by blending a refined kerosene with an isoparaffin and/or a cycloparaffin, exhibits a high volumetric heat of combustion and excellent thermal stability. This combination of properties is especially useful for fueling reusable launch vehicles employing regenerative cooling of engine components.

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Patent Owner(s)

Patent OwnerAddress
JOHANN HALTERMANN LIMITED16717 JACINTOPORT BOULEVARD HOUSTON TX 77015

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Mathur, Indresh Sugar Land, US 20 130

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