The space shuttle is in a 300 km-high circular orbit

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SUMMARY

The discussion focuses on calculating the energy required for the space shuttle to transition from a 300 km circular orbit to a 610 km circular orbit. The relevant equation used is the gravitational potential energy formula, specifically dPE = GMm * (1/(r+h1) - 1/(r+h2)), where G is the gravitational constant, M is the mass of Earth, and m is the mass of the shuttle. The final calculations yield approximately 2.1 x 10^11 J using both the potential energy formula and the simplified mgh approach, confirming that both methods provide consistent results for the energy required.

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mookie84
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Homework Statement



The space shuttle is in a 300 km-high circular orbit. It needs to reach a 610 km-high circular orbit to catch the Hubble Space Telescope for repairs. The shuttle's mass is 7.00×10^4 kg.

Homework Equations


½(-G(M-earth)(M-telescope))(1/r2 –1/r1)
G=6.67*10^6
Mass of earth=5.98*10^24
Mass of telescope= 7.0*10^4 kg
Radius of earth= 6.98*10^6 m


The Attempt at a Solution


What I did was plug in the numbers to the equation. For r2 I added the radius of Earth + the height needed to be attained (610km). For r1 I added the radius of Earth plus the original height (300km). I keep getting 8.4*10^10 which is the incorrect answer. What am I doing wrong?
 
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what is the question?
 
Sorry about that?
How much energy is required to boost it to the new orbit?
 
The difference in height is small compred to Earth's radius - what does "m g h" give?
 
which mass are you referring too? Earth or the satellite?
 
The shuttle - it's just the same question as lifting a weight on earth.
 
I've tried that it doesn't work. The question is asking me how many joules does it take to move the satellite from 310 km above the surface of Earth to 600 km. When i tried the equation you offered I'm neglecting the Earth's radius and mass which affects the gravitational pull
 
You are taking the radius and mass of the Earth into account in the factor 'g'
g = GM_earth/r_earth^2 = 6.67E-11 * 6E24 / (6.4E6 ^ 2) = 9.8 m/s^2

Potential energy is GMm/r so for the difference in height of 300km and 610km we have

dPE = GMm * ( 1/(r+300km) - 1/(r+610km) )
= 6.67E-11 * 6E24 * 7E4 * ( 1/(6370,000+300,000) - 1/(6370,000+610,000) )
= 6.67E-11 * 6E24 * 7E4 * 6.6E-9 = 1.8 E 11 J

or assuming change in gravity between 300km and 610 km is small and mass of shuttle is small compared to earth.
= m g h = 7E4 * 9.8 * 310,000 = 2.1 E11 J

Since the mass of the shuttle is only given to 1 sig figure the answer 2E11J is the same for both.



=
 

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