(A) Every square meter area facing the Sun, at the distance 1 AU from the Sun, receives radiant power = 1.368 kW. Therefore, what is the total power radiated by the Sun? (B) Imagine a spacecraft at distance d from the Sun, which has a solar panel with area A and efficiency e. (I.e., the solar panel converts this fraction of incident sunlight to electric power.) How much electric power can the solar panel produce for the spacecraft? d = 1.56 AU; A 7.02 m^2; e = 28.5 percent;
(A) Every square meter area facing the Sun, at the distance 1 AU from the Sun, receives radiant power = 1.368 kW. Therefore, what is the total power radiated by the Sun? (B) Imagine a spacecraft at distance d from the Sun, which has a solar panel with area A and efficiency e. (I.e., the solar panel converts this fraction of incident sunlight to electric power.) How much electric power can the solar panel produce for the spacecraft? d = 1.56 AU; A 7.02 m^2; e = 28.5 percent;
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Transcribed Image Text:(A) Every square meter area facing the Sun, at the distance 1 AU
from the Sun, receives radiant power = 1.368 kW. Therefore,
what is the total power radiated by the Sun?
(B) Imagine a spacecraft at distance d from the Sun, which has
a solar panel with area A and efficiency e. (I.e., the solar panel
converts this fraction of incident sunlight to electric power.)
How much electric power can the solar panel produce for the
spacecraft?
d = 1.56 AU; A = 7.02 m^2; e = 28.5 percent;
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