A solar flux of 1400 W/m 2 directly strikes a space vehicle surface which has a solar
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A solar flux of 1400 W/m2 directly strikes a space vehicle surface which has a solar absortivity of 0.4 and thermal emissivity of 0.6. The equilibrium temperature of this surface in space at 0 K is
(a) 300 K
(b) 360 K
(c) 410 K
(d) 467 K
(e) 510 K
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Related Book For 
Heat And Mass Transfer Fundamentals And Applications
ISBN: 9780073398181
5th Edition
Authors: Yunus Cengel, Afshin Ghajar
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