Results of the flight of the spacecraft charging sounding rocket payload are given. The payload was designed to create charging by the emission of both positive ions and electrons. The relationship between environmental parameters and changes in vehicle potential during periods of emission was also studied.
Design, development, and flight of a spacecraft charging sounding rocket payload
1979-01-01
Conference paper
No indication
English
NTIS | 1996
|NTRS | 1996
|Sounding Rocket Payload Recovery Systems
AIAA | 1974
|Sounding Rocket Payload Recovery Systems
NTIS | 1972
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