A system for controlling the potential of a vehicle (rocket or satellite) in flight by use of an emitted current of low energy electrons is described. Diagnostic instruments for measuring the efficacy of such a system are discussed. Results of the use of such a system on a sounding rocket launched into the lower ionosphere are presented.
Vehicle Potential Control by Means of Electron Emission
1975
32 pages
Report
No indication
English
Electron-emission displays demonstrate potential
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