What is the Semimajor Axis and Greatest Distance of the Comet?

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Homework Help Overview

The original poster presents a problem involving the calculation of the semimajor axis and greatest distance of a comet's orbit, using historical observations and Kepler's Third Law. The subject area is celestial mechanics.

Discussion Character

  • Exploratory, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • The original poster attempts to apply Kepler's Third Law to find the semimajor axis and greatest distance of the comet. Some participants question the use of Earth's mass instead of the Sun's mass in the calculations.

Discussion Status

Participants are actively discussing the correct application of Kepler's laws and the necessary constants for the calculations. There is a recognition of the need to correct the mass used in the original calculations, but no consensus has been reached on the final values or methods.

Contextual Notes

The original poster expresses confusion about the calculations and seeks clarification on the correct approach. There are also unrelated questions about Kepler's laws and their application to satellites, indicating a broader interest in the topic.

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Homework Statement


Suppose that a comet that was seen in 545 A.D. by Chinese astronomers was spotted again in year 1937. Assume the time between observations is the period of the comet and take its eccentricity as 0.11. What are (a) the semimajor axis of the comet's orbit and (b) its greatest distance from the Sun?


Homework Equations


Kepler's Third Law
T2= [(4pi2)/(GM)]* a3
G = 6.67e-11
Me = 5.98e24

The Attempt at a Solution



part a:
T = 1937-545 = 1392 (365d*24h*3600s) = 4.38e10 sec
e = 0.11

T2= [(4pi2)/(GM)]* a3
solve for a
a = [T2*[(GM)/(4pi2)]](1/3)
a = [(4.38e10)2*[(6.67e-11*5.98e24)/(4pi2)]](1/3)
a= 2.69e11 m

Part b:
Ra = a + ea
solve for Ra with e and a... but I can't find the correct a in first part of question

Whats going on, where did I go wrong?
 
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You used the Earth's mass - you should be using the sun's mass.
 
phyzguy said:
You used the Earth's mass - you should be using the sun's mass.

:face palm:

Thanks so much.
 
In what way kepler's law affects the motion of the Earth when it goes round the sun.
wil kepler's law apply to man-made satellites also. If so why?
 
In what way kepler's law affects the motion of the Earth when it goes round the sun.
wil kepler's law apply to man-made satellites also. If so why?

Well, Kepler's Laws describe any light particle orbiting a very heavy body. So Earth's orbit about the sun follows Kepler's Laws, as do the orbits of satellites about Earth. Does that answer your question?
 
well ... thanks for your answer about the relation between kepler's law and satellites but could you be more specific, coz its a 30marks question and i need a kind of detailed explanation...
 
I won't write your essay for you. For general information on Kepler's Laws, see Wikipedia or your textbook. If you have any specific questions after doing some research, I'm all ears.
 
How would you obtain the index error of the sextant of the sun "by using its diameter on the arc and off the arc".
kindly give ans. appropriately, coz i know how to just obtain the index error of the sun by using a sextant.
 

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