A review of research and development on the microwave-plasma electrothermal rocket

The microwave-plasma electrothermal rocket (MWPETR) shows promise for spacecraft propulsion and maneuvering, without some of the drawbacks of competitive electric propulsion systems. In the MWPETR, the electric power is first converted to microwave-frequency radiation. In a specially-designed microwave cavity system, the electromagnetic energy of the radiation is transferred to the electrons in a plasma sustained in the working fluid. The resulting high-energy electrons transfer their energy to the atoms and molecules of the working fluid by collisions. The working fluid, thus heated, expands through a nozzle to generate thrust. In the MWPETR, no electrodes are in contact with the working fluid, the energy is transferred into the working fluid by nonthermal mechanisms, and the main requirement for the materials of construction is that the walls of the plasma chamber be insulating and transparent to microwave radiation at operating conditions. In this survey of work on the MWPETR, several experimental configurations are described and compared. Diagnostic methods used in the study are described and compared, including titration, spectroscopy, calorimetry, electric field measurements, gas-dynamic methods, and thrust measurements. Measured and estimated performance efficiencies are reported. Results of computer modeling of the plasma and of the gas flowing from the plasma are summarized.more » 32 references.« less

[1]  M. Hawley,et al.  Dissociation and recombination of oxygen atoms produced in a microwave discharge. Part I. Experiment , 1983 .

[2]  M. Hawley,et al.  A Kinetic Model for the Reactions of Co and H2 to CH4 and C2H2 in a Flow Microwave Discharge Reactor , 1976, IEEE Transactions on Plasma Science.

[3]  J. Asmussen,et al.  Demonstration of a new electrothermal thruster concept , 1984 .

[4]  E. Ekinci,et al.  Hydrogen Dissociation in a Microwave Discharge , 1977 .

[5]  O. Levenspiel Chemical Reaction Engineering , 1972 .

[6]  Jes Asmussen,et al.  Microwave electrothermal thruster performance in helium gas , 1987 .

[7]  W. Steiner The recombination of hydrogen atoms , 1935 .

[8]  Jes Asmussen,et al.  An analysis of electromagnetic coupling and eigenfrequencies for microwave electrothermal thruster discharges , 1987 .

[9]  M. Hawley,et al.  Microwave plasma generation of hydrogen atoms for rocket propulsion , 1981 .

[10]  A. Shapiro The dynamics and thermodynamics of compressible fluid flow. , 1953 .

[11]  J. Hollas,et al.  THE ABSORPTION SPECTRA OF HNO AND DNO , 1962 .

[12]  M. Hawley,et al.  An Experimental Study of Reactions of Co and H2 in a Continuous Flow Microwave Discharge Reactor , 1974 .

[13]  I. Amdur The Recombination of Hydrogen Atoms. II. Relative Recombination Rates of Atomic Hydrogen and Atomic Deuterium , 1935 .

[14]  Jes Asmussen,et al.  Experiments with a microwave electrothermal thruster concept , 1984 .

[15]  Jes Asmussen,et al.  Experimental performance of a microwave electrothermal thruster with high temperature nozzle materials , 1987 .

[16]  J. Ducuing,et al.  Vibrational relaxation of H2 in the range 500–40°K , 1974 .

[17]  M. Hawley,et al.  Behavior of a Microwave Cavity Discharge over a Wide Range of Pressures and Flow Rates , 1978, IEEE Transactions on Plasma Science.

[18]  J. E. Bennett,et al.  The measurement of the rate of recombination of hydrogen atoms at room temperature by means of e. s. r. spectroscopy , 1968, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[19]  J. Asmussen,et al.  The design of a microwave plasma cavity , 1974 .

[20]  Martin C. Hawley,et al.  A computer model for the recombination zone of a microwave-plasma electrothermal rocket , 1987 .

[21]  M. Hawley,et al.  FLOW CALORIMETRY OF ELECTRICAL DISCHARGES , 1988 .