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European Student Moon Orbiter solar electric propulsion subsystem architecture: an all–electric spacecraft

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Figure

Table 1.  T5 GOCE performance
Figure 1.  SEP subsystem architecture option one: high mass, low risk, low cost
Table 2. Comparison between dedicated HCT PPU and a switchbox with and without a gimbal
Table 3. T5 GIT specification (GOCE) Mass
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