REDUCED TOXICITY HYPERGOLIC PROPELLANTS

REDUCED TOXICITY HYPERGOLIC PROPELLANTS

The disclosure described herein is a reduced toxicity rocket propellant comprising a liquid fuel and a liquid oxidizer that ignites spontaneously upon contact with each other. The rocket propellant includes a metal hydride catalyst. Multiple embodiments of the propellant include multiple composition...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MAHAKALI ROHIT, DAMBACH ERIK MICHAEL, SOLOMON YAIR, YAN ALLEN, ANDERSON WILLIAM
Format: Patent
Sprache:eng
Schlagworte:
CHEMISTRY
EXPLOSIVES
EXPLOSIVES OR THERMIC COMPOSITIONS
MANUFACTURE THEREOF
MATCHES
METALLURGY
USE OF SINGLE SUBSTANCES AS EXPLOSIVES
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Beschreibung
Zusammenfassung:The disclosure described herein is a reduced toxicity rocket propellant comprising a liquid fuel and a liquid oxidizer that ignites spontaneously upon contact with each other. The rocket propellant includes a metal hydride catalyst. Multiple embodiments of the propellant include multiple compositions of liquid fuel.