1. The problem statement, all variables and given/known data A space station in outer space has a total surface area of 580m^2 with emissivity of 0.62. The temperature of the outside surface is 156K. The walls are 0.25m thick with an average thermal conductivity of 0.038W/mK. Find the temperature of the inner wall of the space station, assuming that the outside surface radiates into an environmnt that is very cold - essentially at 0.0K. 2. Relevant equations P = kA(delta T)/L P = stefan boltzmann constant * A * emissivity * T^4 3. The attempt at a solution No clue how to start. Can someone lead me to the right direction?