Universal Gravitation and spacecraft

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SUMMARY

The discussion centers on calculating the speed of a spacecraft as it falls towards Earth under the influence of gravity, starting from rest at an infinite distance. The mass of the Earth is specified as M_e=5.97×1024 kg, and the gravitational constant is G = 6.67 x 10-11. The correct speed of the spacecraft when it crashes into Earth is determined to be 11172 m/s, while the speed at a distance of r = 7.337 x 107 m from the center of the Earth is calculated to be 3294 m/s. The confusion arises from the application of gravitational potential energy equations and the initial conditions of the problem.

PREREQUISITES
  • Understanding of gravitational potential energy (U = -GMm/r)
  • Familiarity with kinetic energy equations (k = 1/2 mv2)
  • Knowledge of conservation of mechanical energy principles
  • Basic algebra for solving equations
NEXT STEPS
  • Review gravitational potential energy calculations in physics
  • Study the conservation of energy in gravitational fields
  • Practice problems involving spacecraft trajectories under gravity
  • Explore the implications of starting conditions on energy equations
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Students studying physics, particularly those focusing on mechanics and gravitational forces, as well as educators looking for examples of energy conservation in gravitational contexts.

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Homework Statement



Very far from Earth (r = infinity), a spacecraft has run out of fuel and its kinetic energy is zero. If only the gravitational force of the Earth were to act on it (i.e., neglect the forces from the sun and other solar system objects), the spacecraft would eventually crash into the earth. The mass of the Earth is M_e=5.97×1024 kg and its radius is R_e=6.38×106 m.
G = 6.67 x 10-11

Find the speed V of the spacecraft when it eventually crashes into the earth.

Homework Equations



k = 1/2 mv2

U = -GMm/Re

The Attempt at a Solution



So i found this question fine by doing

ki + Ui = kf + Uf

ki = 0

-GMm/(r + Re) = 1/2mv2 + -GMm/Re

reduce to get

-GM/infinty = 1/2v2 + -GM/Re

0 = 1/2v2 + -62413636.36

v = 11172 m/s



The next part is what i don't get

Now find the spacecraft 's speed when its distance from the center of the Earth is r=x(Re), where x=11.5


so r = 7.337 x 107

Using the same equation

-GM/(r) = 1/2v2 + -GM/Re

-5427272.7 = 1/2v2 + -62413636.36

v = 10675 m/s

but that is wrong.

The right answer is 3294 m/s

to get 3294 m/s you have to do

0 = 1/2v2 + -GM/(r) ...r = 7.337 x 107


This step right here is what i don't get. The Ui should not be zero it should be -GM/(r) and the Uf should be -GM/(Re) not -GM/(r)

I don't get why the way i did it on this part where i got v = 10675 doesn't give me the right answer of 3294 :(
 
Last edited:
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The second part is asking the same as the first part except instead of wanting v when it crashes to Earth, it wants v at xR(E). It is till starting from r=infinity. Why would Uf = -GMm/R(E) when it is not located at R(E)?
 
Oh ok i got it. Thanks. I thought it still wanted it when crashing into Earth from the new r. Mastering Physics is always so wordy :(
 

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