Microwave electrothermal propulsion for space

J. L. Power

IEEE Transactions on Microwave Theory and Techniques · 1992 · 37 citations · 8 references

Concepts

Abstract

The microwave electrothermal thruster (MET) is attractive for medium- or high-power spacecraft propulsion. A propellant gas is heated by passing it through a microwave plasma discharge created in a resonant cavity by tuning either the TM

References

8