Abstract
Introduction I N two previouspaperson the 1-kWhydrazinearcjet, two types of electrostatic probe diagnostics were used at the nozzle exit plane to measure electron density ne , electron temperature Te, ion Mach number, plasma velocity u i , gas temperature Tg , and related quantities. All measurements were performed at 10 A and 50 mg/s propellantmass ow on a NASA Lewis Research Center design,3 at a speci c power of P= P mD 22:4 MJ/kg. These measurements were then compared to the two-temperaturechemicalnonequilibriumnumerical arcjet model of Megli et al. The quantitiesne , Te, and ion Mach numberwere determinedwith a novel quadrupleelectrostatic probe swept across the exit plane,with the probe axis parallel to the ow velocity.1;6 The plasma velocity was measured with a double electrostatic probe using a technique similar to current modulation velocimetry (CMV).2;6 Both radial and axial variations of plasma propertieswere measured and compared to the numerical results. This Note presents further results for P= P mD 19:8 MJ/kg and P= P mD 26:0 MJ/kg (Ref. 6). The arcjet operating conditions are given in Table 1. This range of P= P m is representative of the stable operating range of this arcjet on simulated hydrazine (1 mole N2, 2 moles H2). The speci c impulse is interpolatedfromdata acquired elsewhere on a comparable thruster. The quadruple probe combines the triple probe method of Chen and Sekiguchi, rst applied to electric thruster plumes by Tilley et al.,8;9 with the crossed probe theory of Kanal,10 rst applied to a single-speciesplasma by Johnson andMurphree and to a two-species plasma by Burton and Bufton.1 The quadrupleprobe was rst appled to an electric thruster plume by DelMedico and Burton et al.13 The plasma velocity, assumed to equal the ion velocity u i , is determined by a modi cation of a technique rst developed by Pobst et al., in which the arc current is brie y interruptedand the resulting de cit in electron density is convected at the plasma velocity and either detected optically or by a double time-of- ight (TOF) electrostaticprobe. Radial velocity pro les generatedby this technique are accurate to §500 m/s and provide excellent agreement with those generated by numericalmodeling.
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