Electrodynamic Thrust Performance for Space Solar Satellite Applications

The use of spinning tethers to transfer payloads from low earth orbit (LEO) to geosynchronous earth orbit (GEO) has previously been considered for payload masses up to 4000 kg (4 MT). The construction of the solar power station requires a transfer of 22,568 MT per year from LEO to GEO. This is envis...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Estes, Robert D.
Format:	Report
Sprache:	eng
Schlagworte:	Spacecraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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