CLLARE and Apollo compared

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This page lists significant differences between the CLLARE and Apollo missions, with an emphasis on those differences which explain the drastically reduced cost of CLLARE.

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Feature CLLARE Apollo
Crew size 1 3
Propellants Cryogenic LOX/H2, vacuum specific impulse ~450s Hypergolic Aerozine/Nitrogen tetroxide, vacuum specific impulse ~314s
Lunar lander Open cab lander with life support provided by suit Closed, pressurised lander with own life support system
Total launch mass estimated 10000 kg approximately 45000 kg
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