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A performance level compatible with 30% thrust efficiency at 1500 s specific impulse at 1 mlb (4.45 mN) of thrust was demonstrated with the parallel rail pulsed ablative thruster using Teflon… (More)
A pulsed plasma microthruster system was designed, built, flight qualified, and delivered to the Massachusetts Institute of Technology (MIT) Lincoln Laboratory for installation in the LES-6… (More)
Two completely self contained variable thrust flight prototype plasma propulsion systems using solid teflon as propellant were designed, built and laboratory tested. The impulse bit amplitude of each… (More)
Abstract : Operation of the inverse pinch geometry in underwater electrical discharges, viewed as acoustic sources, has been evaluated. The basic characteristics of the signal radiated (e.g.,… (More)