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Problem 10324.
Sold: 1
last one 30.09.2020
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Uploaded: 05.06.2022
Content: 10324.png 25,56 kB
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Uploaded: 05.06.2022
Content: 10324.png 25,56 kB
Юрий Физик
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Product description
Calculate the linear velocity of an artificial Earth satellite at an altitude of 1700 km if its orbit can be considered approximately circular. Take the radius of the Earth 6400 km, acceleration of free fall 10 m/s^2.
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A detailed solution with a brief note of the conditions, formulas and laws used in the solution, the derivation of the calculation formula and the answer.
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