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The end of a cylindrical liquid cryogenic propellant tank
Chapter , Problem 13.6(choose chapter or problem)
The end of a cylindrical liquid cryogenic propellant tank in free space is to be protected from external (solar) radiation by placing a thin metallic shield in front of the tank. Assume the view factor Fts between the tank and the shield is unity; all surfaces are diffuse and gray, and the surroundings are at 0 K. Find the temperature of the shield Ts and the heat flux (W/m2 ) to the end of the tank
Questions & Answers
QUESTION:
The end of a cylindrical liquid cryogenic propellant tank in free space is to be protected from external (solar) radiation by placing a thin metallic shield in front of the tank. Assume the view factor Fts between the tank and the shield is unity; all surfaces are diffuse and gray, and the surroundings are at 0 K. Find the temperature of the shield Ts and the heat flux (W/m2 ) to the end of the tank
ANSWER:Assuming a perfect emitter, the heat radiated outward by the tank is
qout = ??T^4
where ? = emissivity of the tank, T = temperature of the tank, and ? =