Research Article

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

Table 3

Assumed specifications of the lunar lander and the rover.

Lunar lander
Dry mass300 kg
Size (L·W·H)
Specific heat900 kg/J/K
Conductivity20 W/m/K
Heat dissipation (day/night)120 W/10 W
Operating temperature range-20°C ~ 50°C

Rover
Mass25 kg
Size (L·W·H)
Specific heat900 kg/J/K
Heat dissipation (day/night)15 W/0.5 W
Operating temperature range-15°C ~ 45°C