38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2002
DOI: 10.2514/6.2002-4269
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An Experimental Study of a Low-Jitter Pulsed Electromagnetic Plasma Accelerator

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Cited by 3 publications
(9 citation statements)
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“…To provide an azimuthal perturbation to one side of this coil-generated spine axis, we consider the magnetic field of a generalized coaxial plasma gun (CPG) (e.g. Larson, Liebing & Dethlefsen 1966;Scheuer et al 1994;Thio et al 2002) with plasma sheath parameters and run-down phase dynamics identical to a dense plasma focus apparatus (DPF) (see below). A CPG is constructed from a thin, cylindrical anode a few centimetres in length insulated from an outer, concentric cathode.…”
Section: Plasma Scaling Parametersmentioning
confidence: 99%
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“…To provide an azimuthal perturbation to one side of this coil-generated spine axis, we consider the magnetic field of a generalized coaxial plasma gun (CPG) (e.g. Larson, Liebing & Dethlefsen 1966;Scheuer et al 1994;Thio et al 2002) with plasma sheath parameters and run-down phase dynamics identical to a dense plasma focus apparatus (DPF) (see below). A CPG is constructed from a thin, cylindrical anode a few centimetres in length insulated from an outer, concentric cathode.…”
Section: Plasma Scaling Parametersmentioning
confidence: 99%
“…where R is the resistance, C is the capacitance, r is the radial distance and t is the time elapsed since the discharge. Typical values of CPG discharges, V 0 = 6 kV, R = 1 mΩ and C = 330μF, were adopted to approximate this magnetic field (Lindberg & Jacobsen 1961;Larson et al 1966;Schaer 1994;Scheuer et al 1994;Heo & Park 2002;Thio et al 2002;Witherspoon et al 2009). Figures 5(e) and 5( f ) show the simulated electrodynamics of the hardware architecture and demonstrate the feasibility of this configuration to provide the required driving of torsional fan reconnection under proper MHD plasma conditions.…”
Section: Plasma Scaling Parametersmentioning
confidence: 99%
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“…In 1999, Thio et al [45] described an MTF approach that could provide a specific impulse of 7.7 × 10 4 s, power-to-mass ratios up to 1.14 MW∕kg at repetition rate ω 100 Hz, thrust of 340 kN, jet power of 128 GW, and total system mass of 112 tons. Pulsed electromagnetic plasma accelerators were tested [46] and modeled [47] as potential drivers for the plasma liner. The NASA MSFC Advanced Concepts Office conducted a detailed mission analysis for a human-piloted mission to Callisto, summarized in a 140 page analysis of interplanetary mission with human crew using the PJMIF as propulsion [48].…”
Section: B Major Nasa Programsmentioning
confidence: 99%