andoverhockey
New member
- Joined
- Oct 8, 2014
- Messages
- 5
How much work is required to lift a 1300 kg satellite to an altitude of 2*10^6 m above the surface of the Earth? The gravitational force is F=GMm/r^2 , where M is the mass of the Earth (6*10^24 kg), m is the mass of the satellite (1300 kg), and r is the distance between the satellite and the earths center. The radius of the earth is 6.4*10^6 and the gravitational constant, G, is 6.67*10^-11.
Whoo that was quite exhausting typing all of that!
I know that F=GMm/r^2 and also the formula:
Work done = the integrand from a to b of F(x) dx
My work so far:
a = 6.4 x 10^6
b = 10.4 x 10^6
the integrand from a to b of (GMm/r^2) dr
moved the constants outside so.... GMm integrand from a to b of 1/r^2 dr
So now I am confused. Do I take the integral of 1/r^2 then evaluate it from a to b?
Do I just fill in the constants with the numbers and then evaluate?
I keep getting this question wrong so I am not sure what I am doing wrong?
Thanks guys!
Whoo that was quite exhausting typing all of that!
I know that F=GMm/r^2 and also the formula:
Work done = the integrand from a to b of F(x) dx
My work so far:
a = 6.4 x 10^6
b = 10.4 x 10^6
the integrand from a to b of (GMm/r^2) dr
moved the constants outside so.... GMm integrand from a to b of 1/r^2 dr
So now I am confused. Do I take the integral of 1/r^2 then evaluate it from a to b?
Do I just fill in the constants with the numbers and then evaluate?
I keep getting this question wrong so I am not sure what I am doing wrong?
Thanks guys!