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 mass | 300 kg | Size (L·W·H) | | Specific heat | 900 kg/J/K | Conductivity | 20 W/m/K | Heat dissipation (day/night) | 120 W/10 W | Operating temperature range | -20°C ~ 50°C |
| Rover | | Mass | 25 kg | Size (L·W·H) | | Specific heat | 900 kg/J/K | Heat dissipation (day/night) | 15 W/0.5 W | Operating temperature range | -15°C ~ 45°C |
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