CubeSat design for LEO-based Earth science missions

The 2001 University of Washington Space Design class designed and developed a CubeSat platform to accomplish science objectives related to ionospheric modeling. Small satellites (between 1 and 15 kg) show great promise as a low-cost option to perform limited LEO science missions. This paper describe...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Waydo, S., Henry, D., Campbell, M.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Geoscience Global Positioning System Impedance Instruments Low earth orbit satellites Packaging Performance evaluation Plasma applications Plasma measurements Probes
Online-Zugang:	Volltext bestellen
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