Hydroxylammonium nitrate monopropellant with burn rate modifier

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United States of America Patent

PATENT NO 10040730
APP PUB NO 20170166491A1
SERIAL NO

15116039

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Abstract

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A monopropellant includes 30-70% by weight of an oxidizer including hydroxylammonium nitrate, 5-50% by weight of a fuel, and a burn rate modifier in a non-zero amount of up to 3% by weight. The burn rate modifier can be selected from vanadium salts, iron salts, and combinations thereof. The monopropellant is a stable liquid between −20 C and 100 C at ambient pressure.

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Patent Owner(s)

  • AEROJET ROCKETDYNE, INC.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Wucherer, Edward J Woodinville, US 2 38

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