Kepler's laws and proof using angular momentum

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SUMMARY

Kepler's laws of planetary motion are demonstrated through the principles of angular momentum. Kepler's first law asserts that planets, such as Earth, follow elliptical orbits with the sun at one focus, which can be proven using the equation M = dL/dt, indicating that external torque from the sun prevents a planet from leaving its orbital plane. The conservation of angular momentum is utilized to validate Kepler's second law, which states that a planet sweeps out equal areas in equal times, represented mathematically as 2ΔA = |r x Δr|. Additionally, the discussion touches on the percentage difference in Earth's orbital velocities at perihelion and aphelion, specifically at distances of 147.1 million km and 152.1 million km, respectively.

PREREQUISITES
  • Understanding of Kepler's laws of planetary motion
  • Familiarity with angular momentum concepts
  • Basic knowledge of vector mathematics
  • Ability to interpret elliptical orbits in physics
NEXT STEPS
  • Study the derivation of Kepler's first law using angular momentum principles
  • Explore the mathematical proof of Kepler's second law with vector cross products
  • Calculate the percentage difference in orbital velocities at perihelion and aphelion
  • Investigate the implications of angular momentum conservation in celestial mechanics
USEFUL FOR

Students of physics, particularly those studying celestial mechanics, educators teaching planetary motion, and anyone interested in the mathematical foundations of Kepler's laws.

Phy6boii
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a) Kepler's first law states that a planet like Earth displays an elliptical orbit with the sun in focus. Using M = dL/dt, prove that a planet cannot leave its plane of orbit. Note: M here is an externally applied torque that the sun exerts on the planet.
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diagram of the situation described

b) From the above law of angular momentum, it follows that the angular momentum for the planet is conserved. Use this to prove Kepler's second law, which states that at equal time intervals Δt, the traveling beam of a planet covers equal areas ΔA.
Hint: use the representation: 2ΔA = |r x Δr| (proof?), where the origin lies at the focal point of the ellipse.

c) By what percentage do the orbital velocities of the Earth differ approximately at the closest point to the sun (perihelion, rP = 147.1 million km) and at the most remote point (aphelion, rA = 152.1 Million km)

Can someone guide me through these questions please? I'm lost and don't know where to begin with the thought process here. I really want to figure this out
 
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Phy6boii said:
Can someone guide me through these questions please? I'm lost and don't know where to begin with the thought process here. I really want to figure this out
Yes, but this question doesn't belong here. You should start a new thread in the approriate homework forum, which in this case will be https://www.physicsforums.com/forums/introductory-physics-homework.153/

This thread is closed.
 

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