Research Article
A Proposal for Long-Term Missions of Small Lunar Rovers Using an MLI Curtain System
Table 2
Thermal model variables for lunar surface modeling.
| | Modeling variables | Value |
| | Moon surface IR emissivity | 0.97 | | Moon albedo [12] | | | Density of fluff (kg/m3) | 1000 | | Conductivity of fluff (W/m/K) | | | Density of regolith (kg/m3) | 2000 | | Conductivity of regolith (W/m/K) | | | Specific heat of fluff and regolith (J/kg/K) | 1050 | | Imposed heat flow (W/m2) | 0.031 |
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