Reliable, highly reproducible plasma injectors for electrothermal and electrothermal-chemical launchers

• Published in: IEEE transactions on magnetics Vol. 41; no. 1; pp. 355 - 359
• Main Authors: Shafir, N., Zoler, D., Wald, S., Shapira, M.
• Format: Journal Article Conference Proceeding
• Language: English
• Published: New York, NY IEEE 01.01.2005; Institute of Electrical and Electronics Engineers; The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
• Subjects: Ablation; Anodes; Applied sciences; Burning rate; capillary; Charge; Droplets; Electric power generation; Electrothermal launching; Exact sciences and technology; Indication; Injectors; Laboratories; Launchers; Magnetism; Other techniques and industries; Plasma; Plasma density; plasma injector; Plasma properties; Plasma temperature; Propellants; Propulsion; Systems engineering and theory; Temperature control; Testing; Plasma; Launching; capillary; Ablation; plasma injector
• ISSN: 0018-9464; 1941-0069
• DOI: 10.1109/TMAG.2004.839275

The plasma injector is a major component within electrothermal (ET) or electrothermal-chemical (ETC) launcher. Soreq NRC has promoted for years the solid-propellant ETC (SPETC) gun concept, where the generated plasma jet serves to ignite the charge and to control its burning rate (for example, to eliminate the effect of the initial charge temperature on the propellant burning rate). From a system engineering point of view, there is an advantage in using small size plasma injectors. Such injectors have been designed, built, and tested in our laboratory in the past few years. We report about "free jet" (the plasma is injected to the atmosphere and not into propellant charge) experiments performed with certain models of such injectors. These injectors were designed for electrical energies in the range of hundreds of kilojoules and several hundred megawatts. The dependence of the mass losses from the ablative capillary and anode on the total electrical energy and power are presented. Although the limited scope of this presentation one can grasp from these data indications regarding the differences between the thermodynamic properties (temperature, density) of plasma jets produced by capillaries with different geometries, operated at various electrical energies and powers. A comparison between the energy carried by the plasma and metal droplets (resulting from anode melting) may give an indication about the relative contribution of these two factors to the propellant ignition.