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[i]Three entry and postlanding batteries were considered available to supply the total spacecraft power required for entry, parachute descent, and postlanding time. Each battery was assumed to have a 40 A-h capacity until splashdown, at which time the capacity was uprated to 45 A-h. The EPS oxygen consumption rate (lb/hr) = 7.936 x H2[/i]
[i]The CSM shall be habitable for 48 hours and retrievable for 7 days following a water landing. Design Mission Reference Entry and landing .40 hr Consumable Design Mission [list][*]Pre-entry: 0.08 hr [*]Entry: 0.05 hr [*]Recovery: 0.17[/list][/i]
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