Solving Orbital Angle Problem: Worked Examples & Tips for 9a, 9b, and 9c

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SUMMARY

The discussion focuses on solving the orbital angle problem related to Mars, specifically problems 9a, 9b, and 9c. The key solution for problem 9a involves calculating the orbital period of Mars by dividing 300 days by the orbital period, then converting that fraction to radians by multiplying by 2π. The discussion emphasizes that this calculation assumes a circular orbit, and highlights the need for additional data to account for Mars' elliptical orbit for more precise results. Problem 9b has been successfully solved by the user, while assistance is sought for problems 9a and 9c.

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The problem is stated here:

http://i56.tinypic.com/iderfc.jpg

I have included my work until the point I got stuck on.
I have worked out problem 9b) but can't figure out how to solve 9a) and 9c)
Thank you for any help.
 
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diovan said:
The problem is stated here:

http://i56.tinypic.com/iderfc.jpg

I have included my work until the point I got stuck on.
I have worked out problem 9b) but can't figure out how to solve 9a) and 9c)
Thank you for any help.
For part 9a), calculate the orbital period of Mars. Divide 300 days by the orbital period. That number represents the fraction of the orbital period that the Pathfinder was on its trajectory. Convert that fraction to radians by multiplying by 2π.
(Think about it this way. Hypothetically, if it took Pathfinder exactly 1 orbital period (of Mars) to arrive, Mars would have traveled one complete circle, or 2π radians. Of course, it really takes Pathfinder less than 1 orbital period to arrive, and that's where the fraction comes in.) This approximation assumes that Mars travels in a circular orbit however. If you wanted to be more accurate and use Mars' elliptical orbit, more information needs to be given in the problem statement.
 

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