Table 8.5 Chemical Propulsion OTV Mass Summary* Oxygen/Hydrogen Propulsion: Mp = 40,000 kg For the lunar transportation system, the chemical OTV uses two stages of the mass detailed in Table 8.6. The payload delivered to Low Lunar Orbit (LLO) is 35,000 kg. Table 8.6 Electric Propulsion OTV Mass Summary* Xenon Ion (1-MW) - Nuclear Mp = 13,291.54 and Power System Mass = 10 kg/kW The payload delivered to Low Lunar Orbit (LLO) by the Nuclear Electric OTV is 35,000 kg.
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