- [Instructor] A satellite of mass lowercase m orbits Earth
at radius capital R and speed v naught as shown below.
So this has mass lowercase m.
An aerospace engineer decides to launch a second satellite
that is double the mass into the same orbit.
So the same orbit, so this radius is still
gonna be capital R.
And so this satellite, the second satellite,
has a mass of two m.
The mass of Earth is M.
So this is Earth right here, capital M.
What is the speed, lowercase v, of the heavier satellite
in terms of v naught?
And speed you can view as the magnitude of velocity,
and so that's why it's lowercase v
without a vector symbol on it.
And so what we're trying to figure out,
the magnitude of its velocity, in order to stay in orbit.
What is lowercase v going to be equal to?
So pause this video and see if you can figure it out
on your own.
All right so to tackle this, remember the whole reason
why something stays in orbit instead of just going
in a straight line through space is because there is going
to be a constant magnitude centripetal acceleration
towards the center of Earth that keeps turning
I guess you could say the satellite in this circular path.
And we've seen from other videos that the magnitude
of our centripetal acceleration is going to be equal
to the magnitude of our velocity,
and I'll just use this first satellite,
so the magnitude of its velocity squared divided
by our radius, which in this case is a capital R.
But what determines our centripetal acceleration?
Well we can explore Newton's law of gravitation there.
So if we think about the magnitude of the force of gravity,
well that's going to be equal to G,
which is the universal gravitational constant,
times the product of the two masses
that have the force between them,
so the product of the mass of Earth, capital M,
and the mass of this satellite,
I'll just focus on this satellite for now,
divided by the distance between their center
of masses squared.
In this case that is R, capital R, squared.
And if you wanted the centripetal acceleration,
you would just divide force divided by mass.
Remember from Newton's second law,
we know that F is equal to ma.
And so if we're talking about centripetal acceleration,
it's the force of gravity that is causing it.
And so if you wanna solve for centripetal acceleration,
you just divide both sides of these by m.
And so our centripetal acceleration here,
if you divide our force of gravity by lowercase m,
by the mass of the satellite,
our centripetal acceleration is going to be
the universal gravitational constant times the mass of Earth
divided by the radius squared.
And so we could then take this and substitute
it back over here and solve
for the magnitude of our velocity.
So what you're going to have is the universal
gravitational constant times the mass of Earth
divided by the radius squared is equal to
the magnitude of our velocity or the speed squared
divided by capital R.
Now you can multiply both sides by R,
and I'll swap sides as well,
and you're gonna get v naught squared is going to be
equal to capital G times capital M over R.
Or if you take the square root of both sides,
you get v naught is equal to the square root
of the universal gravitational constant
times the mass of Earth divided by the distance
between the center of masses.
Now what's interesting here is,
we see this speed we need in order to maintain this orbit
in no way is it a function of the mass of this satellite.
I don't see a lowercase m anywhere in this expression
on the right-hand side.
And since this is independent of the mass
of the thing that is in orbit,
if you double the mass, if you go from lowercase m
to two times lowercase m,
it does not change the needed orbital speed.
And so what is the speed v of the heavier satellite
in terms of v naught?
It's gonna be the same thing.
We could write v is going to be equal to v naught.
Doesn't matter what you do to the mass here,
you're going to need the same orbital speed.