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N.EO. 2010 KQ
http://www.nasa.gov/topics/solarsyst...d20100527.html
Can anyone explain to me the mechanism.? Velecity of rocket part, relative to the earth , on path almost exactly parallel to the earth's solar orbit path is enough to give one or more solar-earth orbit path distance in 35 years? |
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N.EO. 2010 KQ
On 03/06/10 10:39, N_Cook wrote:
http://www.nasa.gov/topics/solarsyst...d20100527.html Can anyone explain to me the mechanism.? Velecity of rocket part, relative to the earth , on path almost exactly parallel to the earth's solar orbit path is enough to give one or more solar-earth orbit path distance in 35 years? I'm not really clear what you think the problem is? By definition, the Earth is moving fast enough to complete one orbit at one AU from the Sun in one year; so anything which is moving at a comparable speed is also capable of completing an orbit in something like a year. IOW, 2010KQ will return to roughly where it was on May 27th [relative to the Sun] roughly every year, for some value of "rough". If it does so in *exactly* a year, then we will also be there on May 27th, and there is a good chance of *ka-boom*. If it's out by, say, a month, then after twelve orbits it will be out by a year and again there is a decent chance of *ka-boom*. If, as reported, its next near approach is in 2036, then the implication is that it's out by about N/26 of a year, where N is 1, 3, 5, 7, 9 or 11, ie roughly 2, 6, 10, 14, 18 or 22 weeks. Note that the Earth's speed in orbit is 2 pi AU/year, so a two-week error corresponds to a difference in speed of pi/13 AU/year, or about 1 km/s -- not much faster than Concorde, and rather slow in terms of rockets and things in orbit. Of course, this is an average over the orbit, and depends on the eccentricity of the orbit; and a small difference in speed is not the same as a small relative velocity. Details left as an exercise .... After the 2036 approach, its orbit is likely to change, perhaps quite dramatically if the approach is very near [eg, sub- lunar]; so the following near approach is likely to be after some different number of years, up or down. But it will continue to be an occasional visitor until either it hits us or it passes close to some other planet [and changes orbit] or, if it survives long enough, perturbations from [eg] Jupiter affect it enough to shift its orbit well away from ours. -- Andy Walker Nottingham |
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N.EO. 2010 KQ
Andy Walker wrote in message
news:z_LNn.1191$jL2.1125@hurricane... On 03/06/10 10:39, N_Cook wrote: http://www.nasa.gov/topics/solarsyst...d20100527.html Can anyone explain to me the mechanism.? Velecity of rocket part, relative to the earth , on path almost exactly parallel to the earth's solar orbit path is enough to give one or more solar-earth orbit path distance in 35 years? I'm not really clear what you think the problem is? By definition, the Earth is moving fast enough to complete one orbit at one AU from the Sun in one year; so anything which is moving at a comparable speed is also capable of completing an orbit in something like a year. IOW, 2010KQ will return to roughly where it was on May 27th [relative to the Sun] roughly every year, for some value of "rough". If it does so in *exactly* a year, then we will also be there on May 27th, and there is a good chance of *ka-boom*. If it's out by, say, a month, then after twelve orbits it will be out by a year and again there is a decent chance of *ka-boom*. If, as reported, its next near approach is in 2036, then the implication is that it's out by about N/26 of a year, where N is 1, 3, 5, 7, 9 or 11, ie roughly 2, 6, 10, 14, 18 or 22 weeks. Note that the Earth's speed in orbit is 2 pi AU/year, so a two-week error corresponds to a difference in speed of pi/13 AU/year, or about 1 km/s -- not much faster than Concorde, and rather slow in terms of rockets and things in orbit. Of course, this is an average over the orbit, and depends on the eccentricity of the orbit; and a small difference in speed is not the same as a small relative velocity. Details left as an exercise .... After the 2036 approach, its orbit is likely to change, perhaps quite dramatically if the approach is very near [eg, sub- lunar]; so the following near approach is likely to be after some different number of years, up or down. But it will continue to be an occasional visitor until either it hits us or it passes close to some other planet [and changes orbit] or, if it survives long enough, perturbations from [eg] Jupiter affect it enough to shift its orbit well away from ours. -- Andy Walker Nottingham So someone arranges for something quite massive and velocity enough to leave earth's gravity and in a direction near enough exactly parallel to the tangent of the earth's orbit. Knowing that a few decades later it will have travelled AU*2*Pi to likely hit the earth at much the same relative speed. That sounds like gross incompetence to me |
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N.EO. 2010 KQ
On 03/06/10 12:47, N_Cook wrote:
So someone arranges for something quite massive and velocity enough to leave earth's gravity and in a direction near enough exactly parallel to the tangent of the earth's orbit. Actually, to judge from the diagram on the page you referred to, it came in at a reasonable angle and went out roughly parallel; tho' there isn't really enough information there to be sure. But no matter. ... Knowing that a few decades later it will have travelled AU*2*Pi to likely hit the earth at much the same relative speed. That sounds like gross incompetence to me ... Well, it's a feature of closed orbits in a two-body [eg Sun/planet or Sun/spacecraft] system that the bodies keep coming back to the same point with the same velocities. Any changes are due to perturbations, from [eg] Jupiter and/or from near-encounters with [eg] Earth. So it's not so much incompetence as inevitable, unless the spacecraft can either be aimed at some other planet on launch or retain enough fuel to be steered off when well away from Earth. It's not going to matter to us, anyway. Whether 2010 KQ is a stray spacecraft or a genuine asteroid, it's too small to survive its trip through our atmosphere and do serious damage on the ground. -- Andy Walker Nottingham |
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