CLLARE and Apollo compared

From CSTART Wiki

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.

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