A number of phenomena observed on the first orbiting Meteosat satellite attributed to spacecraft charging effects are considered. Design analysis, correlation of anomalies with space environmental data, on ground tests with an engineering model spacecraft, tests on the validity of improvements, and installation of suitable monitors for the second improved flight satellite are discussed.
Meteosat spacecraft charging investigation
1980-10-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Tema Archiv | 1985
|Meteosat Second Generation: CFRP-Structures for High Precision Optical Spacecraft Instruments
British Library Conference Proceedings | 1999
|Meteosat First Generation Spacecraft Power System Design Evolution & In-Orbit Performance Features
British Library Online Contents | 1998
|Meteosat First Generation Spacecraft Power System Design Evolution & In-Orbit Performance Features
British Library Conference Proceedings | 1998
|Tema Archiv | 1979
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