Potential Energy and Velocity of a Spaceship

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SUMMARY

The discussion focuses on calculating the potential energy and velocity of a spaceship traveling from Earth to the Moon. The minimum speed required to reach the Moon is established as vmin = 11068 m/s, while an initial attempt at v = 5534 m/s results in a distance of 8.44 x 106 meters from the Earth's center. The key equations utilized include the conservation of energy principle, ΔE = 0, and the relationship between potential and kinetic energy, U1 + K1 = U2 + K2. The discussion highlights the importance of accurately accounting for gravitational potential energy at both celestial bodies.

PREREQUISITES
  • Understanding of gravitational potential energy and kinetic energy concepts
  • Familiarity with the conservation of energy principle in physics
  • Basic knowledge of celestial mechanics and distances between Earth and Moon
  • Ability to perform calculations involving large numbers and scientific notation
NEXT STEPS
  • Study the derivation of gravitational potential energy equations for celestial bodies
  • Learn about the implications of escape velocity in space travel
  • Explore the concept of energy conservation in multi-body systems
  • Investigate the effects of varying speeds on trajectory and energy calculations
USEFUL FOR

Students studying physics, aerospace engineers, and anyone interested in the mechanics of space travel and energy conservation principles.

Drakkith
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Homework Statement


You plan to take a trip to the moon. Since you do not have a traditional spaceship with rockets, you will need to leave the Earth with enough speed to make it to the moon. Some information that will help during this problem:mearth = 5.9742 x 1024 kg
rearth = 6.3781 x 106 m
mmoon = 7.36 x 1022 kg
rmoon = 1.7374 x 106 m
dearth to moon = 3.844 x 108 m (center to center)
G = 6.67428 x 10-11 N-m2/kg21)On your first attempt you leave the surface of the Earth at v = 5534 m/s. How far from the center of the Earth will you get?
2) Since that is not far enough, you consult a friend who calculates (correctly) the minimum speed needed as vmin = 11068 m/s. If you leave the surface of the Earth at this speed, how fast will you be moving at the surface of the moon? Hint carefully write out an expression for the potential and kinetic energy of the ship on the surface of earth, and on the surface of moon. Be sure to include the gravitational potential energy of the Earth even when the ship is at the surface of the moon!

Homework Equations


ΔE = 0
U1+K1 = U2 + K2

The Attempt at a Solution



Found the answer to Q1. It's 8.44x106 meters.

Q2 is where I'm having trouble. I don't know how to set it up. For Q1, ΔE=0 so ΔU + ΔK = 0 as well. And ΔU = U2-U1.

For Q2, I was thinking you would add the potential energy of the spacecraft for both the Earth and the Moon together, like: U1 = U1E + U1M. That would make ΔU = (U2E + U2M) - (U1E + U1M).

Unfortunately my answer using this method appears to be incorrect. Not sure what to do. I made sure to account for the differing distance between the centers of the Earth and Moon, and the distance between the surfaces of each and the center of the other.
 
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In principle, you need to consider the PE wrt the moon in Q1 too, but that shot falls too far short for it to matter.
Please post the details of your attempt on Q2. Can't tell where or if you are going wrong otherwise.
 
haruspex said:
Please post the details of your attempt on Q2. Can't tell where or if you are going wrong otherwise.

Roger. I'll get on that as soon as I can.
 

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