Publications Details

Investigation of hypergolic fuels with hydrogen peroxide

Melof, Brian M.; Grubelich, Mark C.

A low toxicity, high performance, hypergolic, bipropellant system is desired to replace conventional nitrogen tetroxide (NTO) and hydrazine propulsion systems. Hydrogen peroxide exothermically decomposes to water, and oxygen, making it an ideal oxidizer for more environmentally friendly propulsion systems. Unfortunately, the choice of fuel for such systems is not as clear. Many factors such as ignition delay, performance, toxicity, storability, and cost must be considered. Numerous candidate fuels and fuel/catalyst mixtures were screened using a simple laboratory setup and visual observation. A mixture of ethanolamine and 1% copper (II) chloride was found to rapidly ignite with 90% hydrogen peroxide. Hydrogen peroxide and ethanolamine are much less toxic than NTO and hydrazine. Hydrogen peroxide and ethanolamine have a calculated specific impulse of 245 seconds compared to 284 seconds for NTO and monomethyl hydrazine. A low-freezing blend of furfuryl alcohol (47.5%), ethanolamine (47.5%), and copper (II) chloride (5%) was successfully test fired in a small rocket engine with both 90% and 99% hydrogen peroxide. Hypergolic ignition of this mixture was achieved with 70% hydrogen peroxide. Our quest for a non-toxic hypergol began by researching the literature. Most current low freezing points, exhibit good performance, and are non-toxic compared to hydrazines.1 Unfortunately, hypergolic ignition was only achieved after adding a large amount (>10%) of manganese based catalyst.2-4 Metallic catalysts are toxic and impair performance, so low concentrations are desired. In addition, an insoluble catalyst may not remain in uniform suspension, converting a hypergolic fuel into one with inconsistent age related performance. We wanted to find a fuel that was hypergolic by itself, or that could be made so with a much smaller addition of metallic catalyst.