Performance of a Hydrogen Pulsed Electrothermal Thruster. Strategic Defense Initiative Organization Innovative Science and Technology. SBIR. Phase 1.

reportActive / Technical Report | Accession Number: ADA191999 | Open PDF

Abstract:

This report describes effort to determine the technical feasibility of measuring the performance of a pulsed electrothermal thruster on liquid hydrogen propellant. The design of a 5 kW thruster is presented, including the capacitive pulse forming network, arc discharge characteristics, nozzle performance and predicted specific impulse and thrust. A thermal model is discussed which treats and solves the problem of liquid hydrogen it is concluded that a Phase II test should concentrate on water andor hydrazine, and liquid hydrogen testing should be postponed to Phase III. Keywords Electric propulsion, Pulsed electrothermal propulsion Liquid hydrogen propellant.

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