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Showing 1 to 1 of 1 for “"LOX/ethanol"”.
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Preliminary design of a 1 kN liquid propellant rocket engine testing platform
… propellants, specifically liquid oxygen and ethanol, are pressure-fed using gaseous nitrogen. The test platform supports engine thrust values up to 1 kN, as well as varying oxidizer/fuel ratios up to 4.0 and varying ethanol concentrations between 70 and 100%. The test platform will integrate …