Thus, in the worst case the thrustor efficiency would be 0.986 of the maximum theoretical efficiency obtainable with particles of a single size. It is expected that a high voltage colloid thrustor now being investigated will permit evaluation of other parameters that have not yet been evaluated and that greatly effect thrustor performance (e.g., propellant utilization, power losses, beam current).
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DlETMAR E. ROTHE (1965) studied this question.
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