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An earth-orbiting satellite has solar energy–collecting panels with a
total area of 4.0 m2 . If the sun’s radiation is perpendicular
to the panels and is completely absorbed, find the average solar power
absorbed and the average radiation-pressure force.

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An earth-orbiting satellite has solar energy–collecting panels with a total area of 4.0 m2 . If the sun’s radiation is perpendicular to the panels and is completely absorbed, find the average solar power absorbed and the average radiation-pressure force.