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Propellant Weight/Spacecraft Weight 32 deg Plane Change

O Solar Electric ■ Nuclear Electric

Figure 5.17. Ratio of total propellant weight to satellite weight for solar and nuclear electric propulsion.

Table 5.13. Ratio of total propellant weight to satellite weight for an FDL-7 C/D hypersonic glider with a 32-degree plane change capability and two satellite weights.
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