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![]() Small asteroid misses Earth by only four thousand miles http://www.newscientist.com/news/news.jsp?id=ns99996307 Jim Oberg asks -- were there any other possibile sensors thatr might have detected (but not identified) this bogie? Visual? Radar? IR? Asteroid shaves past Earth's atmosphere 13:59 23 August 04 NewScientist.com news service The closest observed asteroid yet to skim past the Earth without hitting the atmosphere, was reported by astronomers on Sunday. The previously unknown object, spanning five to 10 metres across, has been named 2004 FU162. It streaked across the sky just 6500 kilometres - roughly the radius of the Earth - above the ground on 31 March, although details have only now emerged. |
#2
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"Jim Oberg" wrote in message ...
Small asteroid misses Earth by only four thousand miles http://www.newscientist.com/news/news.jsp?id=ns99996307 Jim Oberg asks -- were there any other possibile sensors thatr might have detected (but not identified) this bogie? Visual? Radar? IR? Depends where it's coming from. Earthbound visual detectors are useless for objects approaching from the daylight side of Earth, since no reflected sunlight is visible. Radar and IR are better, but not many have enough resolving power to detect a 5-10m object. Something that size didn't/doesn't pose anything but a very localized risk anyway. Rick Asteroid shaves past Earth's atmosphere 13:59 23 August 04 NewScientist.com news service The closest observed asteroid yet to skim past the Earth without hitting the atmosphere, was reported by astronomers on Sunday. The previously unknown object, spanning five to 10 metres across, has been named 2004 FU162. It streaked across the sky just 6500 kilometres - roughly the radius of the Earth - above the ground on 31 March, although details have only now emerged. |
#3
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![]() "Rick" wrote in message ... "Jim Oberg" wrote in message ... Small asteroid misses Earth by only four thousand miles http://www.newscientist.com/news/news.jsp?id=ns99996307 Jim Oberg asks -- were there any other possibile sensors thatr might have detected (but not identified) this bogie? Visual? Radar? IR? Depends where it's coming from. Earthbound visual detectors are useless for objects approaching from the daylight side of Earth, since no reflected sunlight is visible. Radar and IR are better, but not many have enough resolving power to detect a 5-10m object. Something that size didn't/doesn't pose anything but a very localized risk anyway. Rick Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. |
#4
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![]() "redneckj" wrote in message news:bNsWc.44518 snip Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. snip Totally, what a great way to do some research then to have an asteroid orbiting the earth, up close and personal. I wonder what sized body it would take before it had an effect on the earth, much like the moon does? BV. |
#5
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"Benign Vanilla" wrote in message ...
"redneckj" wrote in message news:bNsWc.44518 snip Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. snip Totally, what a great way to do some research then to have an asteroid orbiting the earth, up close and personal. I wonder what sized body it would take before it had an effect on the earth, much like the moon does? BV. Capture to reentry might be easier. But any capture for research and analysis is no more useful than all the meteorite analysis already done. Capture for semi commercial exploitation would be a MASSIVE breakthrough. |
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In sci.space.policy Benign Vanilla wrote:
"redneckj" wrote in message news:bNsWc.44518 snip Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. snip Totally, what a great way to do some research then to have an asteroid orbiting the earth, up close and personal. I wonder what sized body it would take before it had an effect on the earth, much like the moon does? Approximately moon sized ;-) Well, ok, it might be small moon sized but not a "pebble" sized. BV. -- Sander +++ Out of cheese error +++ |
#7
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"redneckj" wrote in message
... Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. Oh, God, yes. I'd rather see something like that before I die than men on Mars. Men on Mars may not necessarily lead on to anything else, in the same manner as Apollo. But retrieval of space resources to HEO would to me mean that we were starting the process of being in space to stay. -- Regards, Mike Combs ---------------------------------------------------------------------- Member of the National Non-sequitur Society. We may not make much sense, but we do like pizza. |
#8
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![]() redneckj wrote: "Rick" wrote in message ... "Jim Oberg" wrote in message ... Small asteroid misses Earth by only four thousand miles http://www.newscientist.com/news/news.jsp?id=ns99996307 Jim Oberg asks -- were there any other possibile sensors thatr might have detected (but not identified) this bogie? Visual? Radar? IR? Depends where it's coming from. Earthbound visual detectors are useless for objects approaching from the daylight side of Earth, since no reflected sunlight is visible. Radar and IR are better, but not many have enough resolving power to detect a 5-10m object. Something that size didn't/doesn't pose anything but a very localized risk anyway. Rick Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. Went by kind of quickly: V inf was 10.84 km/sec and V perigee 13.39 km/sec V circular orbit at that altitude is 5.57 and escape 7.87 km/sec. You would need 5.23 km/sec delta vee or more to capture it. http://neo.jpl.nasa.gov/cgi-bin/neo_...how=1&from=120 There are much nicer asteroids in terms of delta vee. The above website allows you to sort close approaches by relative velocity, distance, etc. -- Hop David http://clowder.net/hop/index.html |
#9
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![]() "Hop David" wrote in message ... redneckj wrote: Sounds like an ideal type body for asteroid material return. 300-1,000 tons of material if you can figure a capture to orbit method. Went by kind of quickly: V inf was 10.84 km/sec and V perigee 13.39 km/sec V circular orbit at that altitude is 5.57 and escape 7.87 km/sec. You would need 5.23 km/sec delta vee or more to capture it. http://neo.jpl.nasa.gov/cgi-bin/neo_...how=1&from=120 There are much nicer asteroids in terms of delta vee. The above website allows you to sort close approaches by relative velocity, distance, etc. That vee is most inconvenient for the purpose. My mental picture was of an object with about 1 km/sec at infinity. Perhaps 200 m/sec over escape at perigee. I was thinking of capture to high eliptical orbit. Still a lot of vee to rendezvous each time, and too much Van Allen exposure, but doable. Maybe another body at another time. -- Hop David http://clowder.net/hop/index.html |
#10
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![]() redneckj wrote: Went by kind of quickly: V inf was 10.84 km/sec and V perigee 13.39 km/sec V circular orbit at that altitude is 5.57 and escape 7.87 km/sec. You would need 5.23 km/sec delta vee or more to capture it. http://neo.jpl.nasa.gov/cgi-bin/neo_...how=1&from=120 There are much nicer asteroids in terms of delta vee. The above website allows you to sort close approaches by relative velocity, distance, etc. That vee is most inconvenient for the purpose. My mental picture was of an object with about 1 km/sec at infinity. Perhaps 200 m/sec over escape at perigee. I was thinking of capture to high eliptical orbit. My mental picture as well, with a slight alteration: The perigee would more likely be between 1 and 3 lunar distances (More than 3 LD and it's very easy to perturb it out of earth's Sphere Of Influence). At higher altitudes it might be easier to come up with the delta vee to nudge it into an elliptical orbit. Still a lot of vee to rendezvous each time, and too much Van Allen exposure, but doable. Maybe another body at another time. Using the same site I cited earlier: http://neo.jpl.nasa.gov/cgi-bin/neo_...Table& show=1 To get above page I chose Sort by relative velocity H=24 Future only Ascendng Sort 20 rows per page max Nominal dist. = .1 AU There are some asteroids the size of a basketball, which aren't worth the effort. The H=24 makes it likely the asteroid has a diameter exceeding 50 meters For these the minimum V inf is around 1.5 km/sec. You can get much lower V inf if you expand Nominal dist.= .2 AU but then it would take some delta vee to bring it within Earth's Sphere Of Influence. (I chose 20 rows per page because "show full table" takes awhile to download even with DSL) The best resource on NEOs is the jpl website in my opinion. Yeoman, Baalke et al deserve some Kudos. Using MADMEN you can use fission or solar energy and asteroid material as reaction mass http://www.space.com/businesstechnol...ed_040519.html So it doesn't have to be hugely expensive to change an asteroid's velocity. -- Hop David http://clowder.net/hop/index.html |
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