Abstract
A Hall Effect Thruster propelled by water vapour is investigated at the Imperial Plasma Propulsion Laboratory. For that purpose, a water vapour feed system is designed, optimized and tested, with the major objective of keeping water in vapour state at all times. This system primarily consists of a mass flow controller, a flow restrictor, and a heating and pressure monitor system capable of identifying under which conditions water condensation occurs. A hanging pendulum thrust balance is used to measure the thrust on the power range of Pd=600–1600 W. Different magnetic field strengths and mass flows are investigated to determine the conditions in which the highest efficiency can be achieved. Then, a comparison between water vapour and oxygen (intended to be the propellant of a water electrolysis Hall Effect Thruster) is included. The results show that oxygen is approximately 20% more efficient than water vapour under the same operating conditions. Overall, the highest thrust measurement recorded with water vapour was 20.0±0.2 mN; with a specific impulse of 2039±20 s and an anode efficiency of 12.5±0.3% at the largest discharge power of investigation (Pd=1600±1 W).
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