"A prime example of what would be faced on the moon and Mars is exhibited on the Shuttle. The entire payload bay door inner surfaces are radiators to get rid of heat. Heating is not a problem, cooling is. "<br /><br />On the moon, yes, on Mars, no. The shuttle has to radiate a lot of heat because it is above the atmosphere, receiving about 1.4 times the solar flux we receive on the surface at the equator on a sunny day. <br /><br />Earth normal solar flux on the surface at the equator on a sunny day is still pretty dang intense for anybody but camels. 1.4 times that is broiling. So, in earth orbit, or on the moon, cooling is the main problem, except of course during lunar night, when temperatures are hundreds of degrees below zero, which is when heating IS a huge issue and nuclear power would be essential to keeping one's blood flowing.<br /><br />On or near Mars, however, heating is always an issue. Mars receives .44 of earth normal solar flux, which is about what you get at about 66 degrees north or south latitude: i.e. the latitude that defines the arctic and antarctic circles.... So, once again, nuclear power's cogeneration abilities are essential to the mission application and solar's inability to compete places it at a rather massive disadvantage. Studies cited previously of comparing nuke vs solar only look at electrical loads. They do not look at heating loads for a martian base, and here I believe that nuclear power wins hands down.