Object in elliptical orbit around another object

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SUMMARY

The discussion centers on calculating the difference in total mechanical energy for a satellite, Little Bird, in an elliptical orbit around a large spaceship, Big Bird. The masses are 7.496×1011 kg for Big Bird and 1000 kg for Little Bird, with closest and farthest distances of 5 km and 40 km, respectively. The relevant equations include kinetic energy (K = 1/2mv2) and gravitational potential energy (U = -Gmm/r). The user seeks clarification on applying these equations to find the energy difference between the two orbital positions.

PREREQUISITES
  • Understanding of gravitational potential energy and kinetic energy equations
  • Familiarity with the concept of elliptical orbits
  • Knowledge of the gravitational constant (G)
  • Ability to perform unit conversions (e.g., km to m)
NEXT STEPS
  • Study the principles of elliptical orbits in celestial mechanics
  • Learn how to apply conservation of mechanical energy in orbital dynamics
  • Explore the calculation of orbital velocities using gravitational equations
  • Investigate the implications of mass and distance on gravitational forces
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Students in physics or astronomy, educators teaching orbital mechanics, and anyone interested in the dynamics of satellite motion in space.

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Homework Statement



In a science fiction story, humans have built a large spherical spaceship for an interstellar journey of many generations; they have christened their ship Big Bird.

The mass of Big Bird is 7.496×1011 kg (the mass of an aircraft carrier is about 10^8 kg). Most of Big Bird's journey takes place at constant speed through the vacuum of interstellar space.

Big Bird is accompanied on its journey by a small satellite which is held in orbit about Big Bird solely by Big Bird's gravitational attraction. The satellite is called Little Bird and has a mass of 1000 kg.

Little Bird is in an elliptical orbit about Big Bird; the distance of closest approach is 5 km and the greatest separation distance is 40 km.

Find the difference in total mechanical energy for the system; i.e. mechanical energy at maximum separation minus mechanical energy at closest approach.

Homework Equations



E = K + U

K = 1/2mv2

U = -Gmm/r

The Attempt at a Solution



I am a little confused on this problem. i only seem to know the equation for V for a circular orbit so i am not sure how to go about this problem.

would i maybe do this mL = mass of little bird and mB = mass of big bird

1/2mLv2 + -GmBmL / r1 - [1/2mv2 + -GmBmL / r2 ]

r1 = 40,000 m
r2 = 5,000 m

Thanks for any suggestions on what to do cause i am completely lost on how to go about this problem.
 
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Mechanical energy should be conserved because no forces are acting on the system, shouldn't it?
 
Yes it should be conserved.

Am i even on the right track to find the difference in total mechanical energy for the system?

I am a little confused on what equations to use i guess.

I thought i should use:

K1 + U1 - (K + U)

Where K1 and U1 are:

1/2mLv2 and GmBmL / r

r = 40,000 m

K and U are:

1/2mLv2 and GmBmL / r

r = 5000 mand v can be found using GmB / r

r = 40,000 for the K1 and r = 5000 for K

Am i on the right track with these equations and using the right "r" for each equation or am i not even close?

Thank you
 

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