#91
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Are you objecting to what I say here? If so, you're really arguing that today's astronomical instruments are no better than the instruments more than three decades ago. In many ways they are not. But searching vast quantities of outer space require speed and quantity more than quality. If "somebody" knew it, it wouldn't take long until we all knew it. You can't keep that a secret for very long. Well... I'm waiting... |
#92
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accelerate towards the Sun and with almost equal magnitude, it is obvious the body needs to be nearly on the axis of rotation of the planets in the invariant plane. Just how does a body that large get into such a strange orbit? |
#93
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On 13 Jul 2006 06:14:32 -0700, "George Dishman"
Gave us: George Dishman wrote: No. Let's be clear. We were talking of the Pioneer anomaly which is a linear, constant acceleration relative to the Sun. ... I have also suggested you try to work out where the extra mass would need to be because you will quickly find that there is no possible location that can produce the effect, ... There is no way to produce a constant acceleration with a single extra body but as a lunch-time excercise I tried to find the optimum solution. Since both craft accelerate towards the Sun and with almost equal magnitude, it is obvious the body needs to be nearly on the axis of rotation of the planets in the invariant plane. The primary study of Pioneer 10 covered a heliocentric range of 40 AU to 60 AU so I first found the range to the body that would produce equal acceleration at those two craft ranges. The answer is 50.6 AU. Then I found the mass need to produce an average acceleration of 8.74*10^-8 cm/s^s over the range which turns out to be 2.09*10^25 kg or 1604 times the mass of Pluto. The resulting acceleration is 7.74 *10^-8 cm/s^s at the ends of the data track and peaks at 9.38*10^-8 cm/s^s at 36 AU, a significantly greater variation than is observed. Assuming a density similar to Pluto, the object would actually be 11 times the diameter and appear 9 times larger as it would be slightly farther away than Pluto's orbit of 39 AU. Allowing for that increased range, and assuming a comparable albedo, it would still be about 50 times brighter than Pluto. With a mass of 1600 times that of Pluto, the influence on the orbits of the outer planets would be significant. In other words, it is NOT possible for any such body to exist! |
#94
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On 13 Jul 2006 08:55:26 -0700, "Hurt"
Gave us: One has to get pretty close to Earth in space before one can see the Pyramids, and they are ****ing huge! So are there Pyramids on Mars Roy? Ruins on the Moon? Jeez. Do you ever stay on topic? YOU were talking about being able (or not) to see the man made artifacts that were left behind there, including Lunar Module bases. I mentioned that from Earth it would not be possible due to the already known fact of how far it is. The proof is that we cannot see the pyramids from space until we get fairly close to earth. It has not a goddamned thing to do with your kootard crap about pyramids on Mars. |
#95
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#96
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On 13 Jul 2006 09:49:00 -0700, "Hurt"
Gave us: Remember, "objects in mirror are closer than they appear". You are an IDIOT! Chill with the "we don't know the distances" CRAP! |
#97
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On 13 Jul 2006 15:37:21 -0700, "Hurt"
Gave us: Well... I'm waiting... Well... You're retarded too... |
#98
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"Hurt" wrote in message ups.com... accelerate towards the Sun and with almost equal magnitude, it is obvious the body needs to be nearly on the axis of rotation of the planets in the invariant plane. Just how does a body that large get into such a strange orbit? It gets worse. There is also an acceleration perpendicular to the ecliptic. In this diagram we are on the ecliptic plane, 'A' is the object somewhere roughly over the north pole of the Sun, '*' is the craft at three ranges and I have broken the force at each location into components in the plane and perpendicular: A 24.36 19.60 13.19 6.53 ^ ^ ^ ^ | | | | (Sun) -* -* -* 7.74 9.38 7.74 20AU 36AU 60AU B For the final position, note the upward component is only 6.53 (all accelerations in units of 10^-8 cm/s^2) while for the Sun it is 24.36, that's a downward acceleration of 17.83 relative to the Sun. Combined with the 7.74 towards the Sun, the total relative acceleration would be angled down out of the ecliptic at 66.5 degrees, but we know it is within +/- 1.5 degrees. The solution is to place half the mass at 'A' and the other half at 'B' so the vertical parts cancel while those in the plane add. The obvious question then is how accurate does that have to be to get the direction within +/- 1.5 degrees. The answer is they have to be matched to better than 1.2%. Then you have the problem that these masses cannot just hang there, they must be in orbit. At 50.6 AU the period would be 360 years, but it isn't that simple. A three body solution with a common orbit and the masses on opposite sides of the Sun is not stable. This alignment would have to be purely transient. So you have three big problems: 1. The configuration is unstable. 2. The objects would each be 30 times brighter than Pluto and could not have been missed. 3. Although this is the optimum alignment and range, the anomalous acceleration still varies more than is allowed by observation. Bottom line: gravitational influence of unknown bodies is it is not a credible explanation, these objects simply don't exist. George |
#99
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Hurt wrote: You seem like a pretty smart guy, can you tell me if the measured anomalous acceleration of either Ulysses or Galileo was at or near a Sun-Jupiter LaGrange point? This is interesting. Gots to love the net. http://en.wikipedia.org/wiki/Trojan_asteroids Galileo went into orbit around Jupiter and remained there while Ulysses used a Jupiter slingshot to change into an orbit almost over the solar poles so neither has been anywhere near the Trojan points. The anomaly was measured when the craft was well clear of the planets between the orbits of Uranus and Neptune for Pioneer 11 and starting beyond the orbit of Neptune for Pioneer 10. The software includes the gravitational effects of the Sun, all the planetary systems, our Moon and the major asteroids so Lagrange points are fully modelled anyway. George |
#100
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Galileo went into orbit around Jupiter and remained there while Ulysses used a Jupiter slingshot to change into an orbit almost over the solar poles so neither has been anywhere near the Trojan points. Probably a good thing too. I just mentioned the Trojan Asteroids as a matter of interest as I was looking for the Sun-Jupiter Lagrangian points L1 and L2. http://en.wikipedia.org/wiki/Lagrangian_point Now if there was an external object creating an accelerating force on our Solar System wouldn't it have a tendency to dislodge these Trojan Asteroids? And wouldn't we notice? The anomaly was measured when the craft was well clear of the planets between the orbits of Uranus and Neptune for Pioneer 11 and starting beyond the orbit of Neptune for Pioneer 10. On hyperbolic escape trajectories. |
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