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
We need at least 10 more requests to produce the solution.
0 / 10 have requested this problem solution
The more requests, the faster the answer.