A Proposal for Long-Term Missions of Small Lunar Rovers Using an MLI Curtain System

Table 4

Assumed power consumption of the lunar lander.

Unit	Day (mission profile)	Night (sleep mode)
Main computer	40 W	5 W
Power converter & distributer	40 W	3 W
Communication transponder	20 W	1 W
Battery	0 W	1 W
Location & attitude sensors	5 W	0 W
Lander payloads	15 W	0 W
Total	120 W	10 W