Respuesta :
Answer:
Situation one:
The moon will be experiencing gravitational force in the form of centripetal force, so we equate the two formulas.
Gravitational force = GMm /r²
Centripetal force = mv²/r
Equating,
GMm/r² = mv²/r
v² = GM/r
The first scenario will use the formula v² = GM/r
Situation 2:
The second situation will use the simple distance over time formula for velocity, where the distance will be the circumference and the time will be in seconds.
Answer:
[tex]v = \sqrt{\frac{GM}{r}}[/tex]
[tex]v = 7.59 \times 10^3 m/s[/tex]
Explanation:
As we know that the moon is at distance "r" from the centre of Earth
So we will have
[tex]\frac{GmM}{r^2} = \frac{mv^2}{r}[/tex]
now we have
[tex]v^2 = \frac{GM}{r}[/tex]
[tex]v = \sqrt{\frac{GM}{r}}[/tex]
here
M = mass of moon
r = orbital radius of moon
Now we have to find the speed of satellite which complete the circular orbit of height 150 km
now we have
[tex]radius = (6.37 \times 10^6 + 1.50 \times 10^5) meter[/tex]
times = 90 minutes
[tex]speed = \frac{distance}{time}[/tex]
[tex]v = \frac{2\pi r}{T}[/tex]
[tex]v = \frac{2\pi(6.52 \times 10^6)}{90\times 60}[/tex]
[tex]v = 7.59 \times 10^3 m/s[/tex]