Radiation heat transfer calculations are made for a cylindrical model of a 50th percentile "suited" space man in 7 space configurations: (1) deep space probe, (2) a point 136 miles from the bright side of the moon, (3) a point 136 miles from the surface of the dark side of the moon, (4) a point 500 miles from the surface of the bright side of the earth, (5) a point 500 miles from the surface of the dark side of the earth, (6) a 500 mile circular earth orbit and (7) a 136 mile circular moon orbit. Similarily, radiation heat transfer calculations are made for the same space man model in four hypothetical chamber configurations I, II, III and IV.
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