Preliminary Thermal Design and Analysis of Lunar Lander for Night Survival

Table 6

Optimal radiator area and RHU power for a lunar lander at various landing candidate areas.

Landing candidate area	Latitude	Region	Required area of radiator (m^2)	Required RHU power (W)
1	0°	Highland	0.485	48
2	0°	Lunar mare	0.495	48
3	45°	Highland	0.479	48
4	45°	Lunar mare	0.462	48
5	88.5°	Highland	0.221	50