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An earth- orbiting satellite has a solar...

An earth- orbiting satellite has a solar energy collecting panel with total area `5 m^2` If solar radiations are perpendicular and completely absorbed, the average force associated with the radiation pressure is (Solar constant `= 1.4 k Wm^(-2)` )

A

`2.33xx10^(-3)N`

B

`2.33xx10^(-4)N`

C

`2.33xx10^(-5)N`

D

`2.33xx10^(-6)N`

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The correct Answer is:
To solve the problem of finding the average force associated with the radiation pressure on a solar energy collecting panel of an earth-orbiting satellite, we can follow these steps: ### Step-by-Step Solution: 1. **Identify the Given Data:** - Area of the solar panel, \( A = 5 \, m^2 \) - Solar constant (energy flux), \( S = 1.4 \, kW/m^2 = 1.4 \times 10^3 \, W/m^2 \) - Speed of light, \( c = 3 \times 10^8 \, m/s \) 2. **Calculate the Radiation Pressure:** The radiation pressure \( P \) can be calculated using the formula: \[ P = \frac{S}{c} \] Substituting the values: \[ P = \frac{1.4 \times 10^3 \, W/m^2}{3 \times 10^8 \, m/s} \] \[ P = \frac{1.4 \times 10^3}{3 \times 10^8} = 4.67 \times 10^{-6} \, Pa \] 3. **Calculate the Force:** The force \( F \) associated with the radiation pressure can be calculated using the formula: \[ F = P \times A \] Substituting the values: \[ F = 4.67 \times 10^{-6} \, Pa \times 5 \, m^2 \] \[ F = 2.335 \times 10^{-5} \, N \] 4. **Final Answer:** The average force associated with the radiation pressure is: \[ F \approx 2.33 \times 10^{-5} \, N \]
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