What is the angle of deviation in a plane mirror at normal incidence?
1 answer:
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is the period of orbit.
<u>Explanation: </u>
The equation that is useful in describing satellites motion is Newton form after Kepler's Third Law. The period of the satellite (T) and the average distance to the central body (R) are related as the following equation:
Where,
T is the period of the orbit
R is the average radius of orbit
G is gravitational constant
Here, given data
Substitute the given values, we get T as
Taking square root, we get
Answer:
Option A (69.56 newtons) is the appropriate solution.
Explanation:
According to the question,
On the X-axis,
⇒
or,
On substituting the values, we get
....(equation 1)
On the Y-axis,
⇒
From equation 1, we get