Charge exchange ion formation and motion in mercury ion engine thrust beams
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Engineering topics
Publications and source records attributed to Cole, R. K..
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The interactive effects between a solar electric propulsion system and an electrically propelled scientific spacecraft were examined. The operation of the ion thrusters may impact upon the acquisition and interpretation of data by the science payload of the spacecraft. The effluents from the operation of the electric propulsion unit may also impact upon the operation of the various subsystems of the vehicle. Specific interactive effects were isolated where meaningful levels of interaction may occur. The level of impact upon elements of the science payload and other affected subsystems is examined, and avenues for the reduction or elimination of impact are defined.
Electric propulsion plasma thrust beam and ambient space plasma electrostatic equilibration, considering various charged particle parameters involved in bi-plasma system interactions
Magnetic, electrostatic, space plasma, and electromagnetic contamination levels from electric thruster and solar array
Electron drainage currents from dilute streaming plasmas to positively biased silicon and cadmium sulfide solar cell arrays
Equilibration potentials between dense thrust beam and dilute space plasma measured in wind tunnel
Operation of solar cell arrays in dilute streaming plasmas
Electron deflection instrument for measuring surface electric field strength
Resonance radiation absorption used to study ion engines by detecting neutral atoms in engine exhaust plasma