The present article reports the results of a test campaign performed on a 1 N monopropellant thruster powered by 98% Hydrogen Peroxide. The test campaign comprises firings at different feeding pressures and catalytic bed temperatures. The catalytic bed made of 0.4 mm diameter pellets of -Al2O3 covered by Platinum proved to give fast and repeatable propulsive performance with good decomposition efficiency.

Propulsive Performance of a 1 N 98% Hydrogen Peroxide Thruster

PASINI, ANGELO;PACE, GIOVANNI;
2015-01-01

Abstract

The present article reports the results of a test campaign performed on a 1 N monopropellant thruster powered by 98% Hydrogen Peroxide. The test campaign comprises firings at different feeding pressures and catalytic bed temperatures. The catalytic bed made of 0.4 mm diameter pellets of -Al2O3 covered by Platinum proved to give fast and repeatable propulsive performance with good decomposition efficiency.
2015
978-1-62410-321-6
978-1-62410-321-6
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11568/821794
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