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I notice that figures on various web pages and in books for
the mean radius of the orbits of Saturn, Uranus, Neptune, and Pluto frequently disagree in the third or even the second significant digit. Such a large disagreement between sources surprises me. Is there any any explanation for it? Here are the figures I'm currently using: Mercury 57,910,000 km = 0.3871 AU Venus 108,200,000 km = 0.7233 AU Earth 149,597,870 km = 1 AU Mars 227,940,000 km = 1.5237 AU Jupiter 778,330,000 km = 5.203 AU Saturn 1,429,400,000 km = 9.5388 AU Uranus 2,870,990,000 km = 19.1914 AU Neptune 4,504,300,000 km = 30.0611 AU Pluto 5,913,520,000 km = 39.5294 AU It is always possible that I've made gross errors, as well, so please point out to me whatever you see. :-) -- Jeff, in Minneapolis Subtract 1 from my e-mail address above for my real address. .. |
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Dear Jeff Root:
"Jeff Root" wrote in message om... I notice that figures on various web pages and in books for the mean radius of the orbits of Saturn, Uranus, Neptune, and Pluto frequently disagree in the third or even the second significant digit. Such a large disagreement between sources surprises me. Is there any any explanation for it? Here are the figures I'm currently using: Mercury 57,910,000 km = 0.3871 AU Venus 108,200,000 km = 0.7233 AU Earth 149,597,870 km = 1 AU Mars 227,940,000 km = 1.5237 AU Jupiter 778,330,000 km = 5.203 AU Saturn 1,429,400,000 km = 9.5388 AU Uranus 2,870,990,000 km = 19.1914 AU Neptune 4,504,300,000 km = 30.0611 AU Pluto 5,913,520,000 km = 39.5294 AU URL:http://nssdc.gsfc.nasa.gov/planetary...ble_ratio.html Saturn 1,433,530,000 = 9.58 (three times the eccentricity of Earth) Uranus 2,872,460,000 = 19.20 (nearly three times the eccentricity) Neptune 4,495,060,000 = 30.05 (less eccentric but completes one orbit in 163 years) Pluto 5,869,660,000 = 39.24 (fourteen times as eccentric, one orbit completes in 247 years) These web pages were updated this month. I suspect the variance is due to the difficulty that orbit eccentricity and long periods present in accuracy. My guess. David A. Smith |
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"Jeff Root" wrote in message
om... I notice that figures on various web pages and in books for the mean radius of the orbits of Saturn, Uranus, Neptune, and Pluto frequently disagree in the third or even the second significant digit. Such a large disagreement between sources surprises me. Is there any any explanation for it? Here are the figures I'm currently using: Mercury 57,910,000 km = 0.3871 AU Venus 108,200,000 km = 0.7233 AU Earth 149,597,870 km = 1 AU Mars 227,940,000 km = 1.5237 AU Jupiter 778,330,000 km = 5.203 AU Saturn 1,429,400,000 km = 9.5388 AU Uranus 2,870,990,000 km = 19.1914 AU Neptune 4,504,300,000 km = 30.0611 AU Pluto 5,913,520,000 km = 39.5294 AU It is always possible that I've made gross errors, as well, so please point out to me whatever you see. :-) -- Jeff, in Minneapolis Subtract 1 from my e-mail address above for my real address. I doubt that what follows will fully account for the discrepancies but it is something to keep in mind. The mean orbital radius is often quoted as being equal to the semi-major axis, but this is, in fact, just a very good approximation for orbits with small eccentricity. The full solution is given by ... Mean Orbital Radius = a(1 + (e^2)/2) were a = semi-major axis and e = eccentricity (It is difficult to find a reference for this on-line, but I did find one once. If you would like, I could see if I can dig it up.) |
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David A. Smith replied to Jeff Root:
URL:http://nssdc.gsfc.nasa.gov/planetary...ble_ratio.html I was sure I used the fact sheet pages on that site for the individual planets, just a couple of months ago. But they all have more data on them than I remember. They have exactly what I was looking for-- and eventually found most of, scattered across four or five different sites, including one in German-- all in one place. Maybe I was looking at a mirror site, and the mirror needed re-aluminizing. Thank you! -- Jeff, in Minneapolis .. |
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John Zinni replied to Jeff Root:
The mean orbital radius is often quoted as being equal to the semi-major axis, but this is, in fact, just a very good approximation for orbits with small eccentricity. The full solution is given by ... Mean Orbital Radius = a(1 + (e^2)/2) where a = semi-major axis and e = eccentricity I'm lousy at most aspects of math, but had noticed and wondered about what seemed to be a discrepancy between statements about the meaning of "mean" in this case. I didn't follow up on that puzzlement. Now I will. (It is difficult to find a reference for this on-line, but I did find one once. If you would like, I could see if I can dig it up.) I would like to know. If you can't easily locate the URL, it might be enough if you were to suggest a search term or two in addition to the obvious ones in your first reply. Thank you! -- Jeff, in Minneapolis .. |
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"Jeff Root" wrote in message
m... John Zinni replied to Jeff Root: (It is difficult to find a reference for this on-line, but I did find one once. If you would like, I could see if I can dig it up.) I would like to know. If you can't easily locate the URL, it might be enough if you were to suggest a search term or two in addition to the obvious ones in your first reply. Thank you! Hi Jeff I will give you a brief history (if you will bear with me) of how I found this solution because I think it illustrates well what is going on. The question of "What is the mean 'r' for an elliptic orbit" came up in conversation with a friend in relation to a course we were both taking at the time. "No problem!" I thought to myself (more than a little cocky!), all you need to do is express the equation of an ellipse, with one focus at the origin, in polar form, integrate from 0 to 2Pi and divide by 2Pi (search on something like "mean of a continues function" for this). Well, if you do this, what you come up with is 'b' (that is the semi-MINOR axis) and this contradicted all references I had that the mean orbital radius is 'a' (the semi-MAJOR axis). After re-doing the integration about 4 or 5 times and coming up with the same answer each time, we came to the realization that the mean 'r' for a plain old ellipse and for an elliptic orbit are not the same. The reason for the discrepancy is Kepler's Second Law. That is, for a plain old ellipse, equal weight is given to all values of 'r' but for an elliptic orbit, we know from Kepler's Second Law that at large 'r' the orbital speed is less that at small 'r' (the object hangs out at large values of 'r' for more time than it does at small values of 'r', so large values of 'r' need to be more heavily weighted than the small values of 'r' hence lengthening the mean 'r'). This was what prompted the search for the actual derivation of the value of the mean 'r'. I found this paper. It looks like a problem that was posed in a 2nd or 3rd year math class. It states the problem and gives the solution in the first part. The problem the students had to solve was the rather nasty definite integral involved (If, as you say, you are "lousy at most aspects of math" than the solutions to the definite integral given by three of the students is likely to look like gobbledygook). http://www.math.wisc.edu/~robbin/angelic/anIntegral.pdf Enjoy! John Zinni |
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In article , Jeff Root wrote:
I notice that figures on various web pages and in books for the mean radius of the orbits of Saturn, Uranus, Neptune, and Pluto frequently disagree in the third or even the second significant digit. Such a large disagreement between sources surprises me. Is there any any explanation for it? Here are the figures I'm currently using: Mercury 57,910,000 km = 0.3871 AU Venus 108,200,000 km = 0.7233 AU Earth 149,597,870 km = 1 AU Mars 227,940,000 km = 1.5237 AU Jupiter 778,330,000 km = 5.203 AU Saturn 1,429,400,000 km = 9.5388 AU Uranus 2,870,990,000 km = 19.1914 AU Neptune 4,504,300,000 km = 30.0611 AU Pluto 5,913,520,000 km = 39.5294 AU I"ll bet the reason you see different tabulated values is simply that the orbits aren't constant! The planets perturb each others' orbits, especially Jupiter. So the precise elements you get depends on the time you take the "snapshot". I once wrote a planetarium program that used osculating orbital elements dated from the beginning of 1996. Within a few years, the outer planets' positions were different by up to several arc minutes from the ones my program computed using fixed Keplerian orbits. I'd imagined that the perturbations would be too small to notice, but they really weren't. Cheers Stuart |
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