Essentially, I am trying to design a heat exchanger for a space suit traveling to mars. From my understanding, I assumed that the energy generated from the space suit relates to the astronaut as well as the electrical components. In addition, by comparing the atmosphere of mars to earth, I considered convection to be negligible. As well as the radiation that would be absorbed from the sun since the suit is white and reflective.
And that the only way energy is leaving the suit is by radiation emitted from the heat exchanger. In order to improve the current system, my aim is to make the cooling system lighter and more compact. I chose to design a cross-flow heat exchanger for this reason. From my understanding, it is important to choose a material with high thermal conductivity for efficient heat transfer. I was thinking of aluminum alloys due to its properties, along with water as the coolant.
Now if I want to maintain the inside of the suit as body temperature, I am sort of lost as to what my conditions would be. I know I want to maintain body temperature within the suit, but I am not too sure about my inlet/outlet temperatures, and flow. Should I consider other parameters or heat exchangers as well, and if so, why?