Vehicle charging effects during electron beam emission from the CHARGE-2 experiment

The CHARGE-2 sounding rocket payload has measured the transient and steady-state charging of a spacecraft in LEO during the emission of a low-power electron beam. The electron beam successfully escaped the emitting spacecraft above 240 km, rather than being degraded by the spacecraft's potentia...

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Veröffentlicht in:	Journal of spacecraft and rockets 1990-01, Vol.27 (1), p.25-37
Hauptverfasser:	Myers, Neil B, Raitt, W. John, White, A. Brent, Banks, Peter M, Gilchrist, Brian E, Sasaki, Susumu
Format:	Artikel
Sprache:	eng
Schlagworte:	Electron beams Launch Vehicles And Space Vehicles
Online-Zugang:	Volltext
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