(a)
The power received by the city from the space mirror reflecting light.
(a)
Answer to Problem 60P
The power received by the city from the space mirror reflecting light is
Explanation of Solution
Given info: The diameter of the space mirror is
The formula to calculate the area of space mirror is,
Here,
Substitute
The formula to calculate the net power received by the mirror station is,
Here,
Substitute
The formula to calculate the power received by the city is,
Substitute
Thus, the power received by the city from the space mirror reflecting light is
Conclusion:
Therefore, the power received by the city from the space mirror reflecting light is
(b)
The intensity of light received by the city.
(b)
Answer to Problem 60P
The maximum intensity of light received by the city is
Explanation of Solution
Given info: The diameter of the space mirror is
The formula to calculate the area of space mirror is,
Here,
Substitute
The formula to calculate the net power received by the city is,
Here,
Rewrite the above equation to find the value of
Substitute
Thus, the maximum intensity of light received by the city is
Conclusion:
Therefore, the maximum intensity of light received by the city is
(c)
The percentage of vertical component of the intensity of sunlight at St. Petersburg, when the sun reaches at an angle of
(c)
Answer to Problem 60P
The percentage of vertical component of the intensity of sunlight at St. Petersburg, when the sun reaches at an angle of
Explanation of Solution
Given info: The diameter of the space mirror is
The formula to calculate the intensity of light on earth is,
Substitute
The sunlight reaches the city St. Petersburg when the sun reaches at an angle of
Substitute
The formula to calculate the percentage of
Substitute
Thus, the percentage of vertical component of the intensity of sunlight at St. Petersburg, when the sun reaches at an angle of
Conclusion:
Therefore, the percentage of vertical component of the intensity of sunlight at St. Petersburg, when the sun reaches at an angle of
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Chapter 24 Solutions
Principles of Physics: A Calculus-Based Text
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- A possible means of space flight is to place a perfectly reflecting aluminized sheet into orbit around the Earth and then use the light from the Sun to push this "solar sail." Suppose a sail of area A = 5.20 x 105 m² and mass m = 6,200 kg is placed in orbit facing the Sun. Ignore all gravitational effects and assume a solar intensity of 1,370 W/m². (a) What force (in N) is exerted on the sail? (Enter the magnitude.) N (b) What is the sail's acceleration? (Enter the magnitude in µm/s².) μm/s² (c) Assuming the acceleration calculated in part (b) remains constant, find the time interval (in days) required for the sail to reach the Moon, 3.84 x 108 m away, starting from rest at the Earth. days (d) What If? If the solar sail were initially in Earth orbit at an altitude of 340 km, show that a sail of this mass density could not escape Earth's gravitational pull regardless of size. (Calculate the magnitude of the gravitational field in m/s².) m/s² (e) What would the mass density (in kg/m²) of…arrow_forwardA possible means of space flight is to place a perfectly reflecting aluminized sheet into orbit around the Earth and then use the light from the Sun to push this "solar sail. Suppose a sail of area A 6.30 x 10 m² and mass m - 7,000 kg is placed in orbit facing the Sun. Ignore all gravitational effects and assume a solar intensity of 1,370 W/m² (a) What force (in N) is exerted on the sail? (Enter the magnitude) (b) What is the sail's acceleration? (Enter the magnitude in um/s².) m/s² (c) Assuming the acceleration calculated in part (b) remains constant, find the time interval (in days) required for the sail to reach the Moon, 3.84 x 10 m away, starting from rest at the Earth days (d) What If? If the solar sail were initially in Earth orbit at an altitude of 400 km, show that a sall of this mass density could not escape Earth's gravitational pull regardless of size. (Calculate the magnitude of the gravitational field in m/s².) m/s² (e) What would the mass density (in kg/m²) of the solar…arrow_forwardIn theory, pressure from the sun's radiation could propel a spacecraft outward away from the sun. For a spacecraft of mass = 1340 kg at the same distance from the sun as Earth (150 million km), how much area would a 100% reflecting "sail" need to have in order to balance the sun's force of gravity acting on the spacecraft? For reference, the sun's intensity just outside Earth's atmosphere is 1400 W/m² and the sun's mass is 1,99 x 1030 kg, and the universal gravitational constant G = 6.67 x 10-11 Nm²/kg². Convert your answer to square km (1 km² = 106 m²). A = km²arrow_forward
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