Current status of the microwave arcjet thruster

D. J. Sullivan, J. Kline, C. Philippe, M. M. Micci

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Abstract

The microwave arcjet thruster uses microwave energy to create a free-floating plasma discharge within a microwave resonant cavity. This discharge absorbs the input microwave power and converts it to thermal energy which is then transferred to the flowing propellant gas. The thruster can be operated in a fixed configuration where neither the cavity geometry nor the tuning mechanisms are adjusted; optimization of this geometry for a given propellant results in power coupling in excess of 97%. The prototype has demonstrate its ability to operate in this fixed configuration within a vacuum tank facility where it has been extensively tested using both N2 and NH3. The current design is capable of efficient operation over a wide range of power levels and mass flow rates resulting in representative specific powers of 6.5 MJ/kg for N2 and 77.2 MJ/kg for NH3. Current work is focused on development of a compact power supply, redesign of the current prototype to allow for high temperature operation, and design of a low-mass prototype design which mates the magnetron supply directly to its power coupling probe.

Original languageEnglish (US)
Title of host publication31st Joint Propulsion Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9780000000002
StatePublished - 1995
Event31st Joint Propulsion Conference and Exhibit, 1995 - San Diego, United States
Duration: Jul 10 1995Jul 12 1995

Publication series

Name31st Joint Propulsion Conference and Exhibit

Other

Other31st Joint Propulsion Conference and Exhibit, 1995
CountryUnited States
CitySan Diego
Period7/10/957/12/95

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Control and Systems Engineering
  • Aerospace Engineering

Fingerprint Dive into the research topics of 'Current status of the microwave arcjet thruster'. Together they form a unique fingerprint.

  • Cite this

    Sullivan, D. J., Kline, J., Philippe, C., & Micci, M. M. (1995). Current status of the microwave arcjet thruster. In 31st Joint Propulsion Conference and Exhibit [AIAA-95-3065] (31st Joint Propulsion Conference and Exhibit). American Institute of Aeronautics and Astronautics Inc, AIAA.