Answer:v=\sqrt{\frac{Gm}{r}}
Explanation:
Given
Orbital speed is v
Mass of planet is m
Radius of circular orbit is r
suppose M is the mas of satellite then centripetal force on satellite is equal to the Gravitational Pull.
\frac{Mv^2}{r}=\frac{GMm}{r^2}
where G=gravitational constant
thus on solving we get
v=\sqrt{\frac{Gm}{r}}
Author:
lolagqw5
Rate an answer:
6The orbital speed v of a satellite in a circular orbit of radius r around a planet of mass m should be v = √Gm/r.
Calculation of the orbital speed:
Since
Orbital speed is v
Mass of planet is m
The radius of the circular orbit is r
Here we assume M is the mass of the satellite so the centripetal force on the satellite should be equivalent to the Gravitational Pull.
So,
Mv^2 /r = GMm/r^2
Here
G=gravitational constant
So, v = √Gm/r.
Author:
honeyud4s
Rate an answer:
10Rate an answer:
0Don't worry! There are several alternative approaches you can try to resolve your query. Here are some tips to help you find answers in different ways:
Remember, the process of finding answers often involves persistence, creativity, and an open mind. By exploring various resources, reaching out to others, and being proactive in your search, you increase your chances of finding the information you need. Happy quest for knowledge!