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Introductory Physics Homework Help
Time to Mars (orbit around Sun given perihelion and aphelion)
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[QUOTE="oddjobmj, post: 4492144, member: 127165"] Thank you! It tells me that the T^2/R^3 of the satellite should be the same as for the Earth which is 2.977E-19. It worked out to 516.83 which is actually really close to my original answer but I then had to divide that by 2 to get the time until arrival. [/QUOTE]
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Introductory Physics Homework Help
Time to Mars (orbit around Sun given perihelion and aphelion)
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