SATELLITE DE-ORBITING BY MEANS OF ELECTRODYNAMIC TETHERS...

SATELLITE DE-ORBITING BY MEANS OF ELECTRODYNAMIC TETHERS PART II: SYSTEM CONFIGURATION AND PERFORMANCE

L. IESS, C. BRUNO, C. ULIVIERI, G. VANNARONI
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Volume:
50
Year:
2002
Language:
english
Pages:
10
DOI:
10.1016/s0094-5765(01)00181-3
File:
PDF, 121 KB
english, 2002
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