Modeling and direct thrust measurements of an 8-ghz microwave electrothermal thruster

Jeffrey R. Hopkins, Christopher DeForce, Michael M. Micci, Sven G. Bilén, Silvio G. Chianese

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

3 Scopus citations

Abstract

Fluid mechanics modeling and direct thrust measurements on an 8-GHz microwave electrothermal thruster were performed. Computer modeling involved implementing 2D and 3D simulations of swirl flow dynamics and choked nozzle flow in a cylindrical cavity. These models were run in COMSOL Multiphysics to simulate flow conditions in the thruster and ultimately lead to a fully integrated fluids and electromagnetic model. Experimental work involved redesign of the thruster cavity and construction and testing of a vertical thrust stand. Thrust measurements were taken using ammonia and simulated decomposed hydrazine as propellants. Testing was performed over a range of 100 to 250 W of microwave power input into the thruster.

Original languageEnglish (US)
Title of host publication47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
StatePublished - 2011
Event47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 - San Diego, CA, United States
Duration: Jul 31 2011Aug 3 2011

Publication series

Name47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011

Other

Other47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
Country/TerritoryUnited States
CitySan Diego, CA
Period7/31/118/3/11

All Science Journal Classification (ASJC) codes

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

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