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

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Design category</td><td class="align_center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Radiator area of the lander</td><td class="align_center">3600 cm<sup>2</sup></td></tr><tr><td class="align_left">Radiator area of the rover</td><td class="align_center">640 cm<sup>2</sup></td></tr><tr><td class="align_left">Heat capacity of the RHUs in the lander</td><td class="align_center">20 Watt</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Thermal design result of the lunar lander and the rover.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: A Proposal for Long-Term Missions of Small Lunar Rovers Using an MLI Curtain System 