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.File in questo prodotto:
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