Book ChapterDOI
16. Plasma Problems in Electrical Propulsion
TLDR
In this article, the authors discuss the plasma problems in electrical propulsion, and present several excellent developments of the rationale for electrical propulsion are available, such as: electric propulsion is concerned with plasma of medium to heavy elements, fairly well ionized, and having electron and ion densities in the range of 10 11 -10 15 /cm 3.Abstract:
Publisher Summary This chapter discusses the plasma problems in electrical propulsion. The involvement of plasma physics and technology in the area of space propulsion has occurred because (1) with the exception of nuclear explosions, the electrical or electromagnetic acceleration of conducting matter is the only feasible way of bringing rocket exhausts to the very high velocities necessary for deep space flight with payloads of men and their support equipment; (2) Ionized gas, or plasma, is the most convenient conducting material to use, as by virtue of its usually low density, it can be brought to the requisite velocities without the expenditure of prohibitive increments of energy. Several excellent developments of the rationale for electrical propulsion are available. The field of electric propulsion is concerned with plasma of medium to heavy elements, fairly well ionized, and having electron and ion densities in the range of 10 11 -10 15 /cm 3 .read more
Citations
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Journal ArticleDOI
Anode power deposition in magnetoplasmadynamic thrusters
TL;DR: In this article, anode heat flux and anode fail measurements from a multimegawatt self-field quasi-steady magnetoplasmadynamic (MPD) thruster are presented.
Journal ArticleDOI
Microinstabilities in a 10-Kilowatt Self-Field Magnetoplasmadynamic Thruster
TL;DR: In this paper, the authors provided experimental evidence for the existence of micro-instabilities in a 10-kW-class, self-field magnetoplasmadynamic (MPD) thruster.
Journal ArticleDOI
Instantaneous current and field structure of a gun-driven spheromak for two gun polarities
TL;DR: In this article, the instantaneous structure of the SPHEX spheromak was determined by numerically processing data from insertable Rogowski and magnetic field probes and compared for two modes of gun operation: with the central electrode biased positively and negatively.
Journal ArticleDOI
An Alfvenic reconnecting plasmoid thruster
TL;DR: In this article, a new concept for generation of thrust for space propulsion is introduced, which utilizes a current-sheet instability to spontaneously and continuously create plasmoids via magnetic reconnection, and the generated low-temperature plasma is simulated in a global annular geometry using the extended magnetohydrodynamic model.
Journal ArticleDOI
An Alfvenic reconnecting plasmoid thruster
TL;DR: In this paper, a new concept for the generation of thrust for space propulsion is introduced, which utilizes a current-sheet instability to spontaneously and continuously create plasmoids via magnetic reconnection.
References
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Journal ArticleDOI
Experimental results in high-specific-impulse thermoionic acceleration
Journal ArticleDOI
An energy inventory in a coaxial plasma accelerator driven by a pulse line energy source
TL;DR: In this article, energy measurement in coaxial plasma accelerator determining current, voltage on gun and at open end of pulse line was performed. And the results showed that the current and voltage on the gun were equal.
Journal ArticleDOI
Piezoelectric probe for plasma research
Martin O. Stern,Edward N. Dacus +1 more
TL;DR: A piezoelectric probe has been devised for use in plasma work, where one wishes to measure phenomena of short time duration (micro seconds) giving rise to moderately small pressures (fractions of an atmosphere) as discussed by the authors.
Journal ArticleDOI
Dynamic efficiency of pulsed plasma accelerators
Neville A. Black,Robert G. Jahn +1 more
Journal ArticleDOI
Measurement of ion velocity distributions in low-density plasma beams.
TL;DR: Diagnostic probe for low density plasma beam ion velocity distribution measurement in steady state and pulsed plasma exhausts is described in this paper. But it is not suitable for the measurement of high density ion velocities.