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a Sized for 62° plane change operated over a 32° plane change.

a Sized for 62° plane change operated over a 32° plane change.

Table 5.15. Ratio of total propellant weight to satellite weight for FDL-7 C/D hypersonic glider compared to the hydrogen/oxygen propellant OMV designed for a 32-degree plane change for four launch propulsion systems.

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