Concept includes three major subsystems; energy source, power converter, and ion thrust chamber; diagram of model which, it is believed, results in engine of minimum weight and simplicity; important factors to consider in design and application; problem areas of individual components.
Ion rocket engine systems
Aero Space Eng
Aero/Space Engineering ; 18 , n 4 ; p 67-71 + 75
1959
Aufsatz (Zeitschrift)
Englisch
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