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Considering the number of research satellites that fail or partially fail
due to instrument or other presumably fixable problem, why aren't satellites (whose mission profiles permit) launched to a near enough vicinity of the ISS so that astronouts can go out and fix 'em Surely the sats could also be made fixable? How many 100 Million to Billion dollars sats could have been salvaged this way. Could this be a way to make space colonisation pay? Hey, maybe the sats could be constructed in orbit? It could be a good excuse for geosynchronous and Lagrangian stations too |
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On Sun, 19 Mar 2006 13:55:38 +1100, "BlagooBlanaa"
wrote: Considering the number of research satellites that fail or partially fail due to instrument or other presumably fixable problem, why aren't satellites (whose mission profiles permit) launched to a near enough vicinity of the ISS so that astronouts can go out and fix 'em Does it really strike you as being a good idea to try to send possibly malfunctioning satellites as close to ISS as possible? Are you a curling fan? ![]() How many 100 Million to Billion dollars sats could have been salvaged this way. How many 100 Million to Billion dollars extra would it cost to send satellites to ISS orbit, check the oil, then send them to where they need to be? Could this be a way to make space colonisation pay? Only if you can find a mathematically challenged satellite owner to pay the bill ![]() Dale |
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Dale wrote:
Does it really strike you as being a good idea to try to send possibly malfunctioning satellites as close to ISS as possible? Are you a curling fan? ![]() " 'Close' counts only for horseshoes and hand grenades." |
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On Sun, 19 Mar 2006 10:12:35 GMT, Monte Davis wrote:
" 'Close' counts only for horseshoes and hand grenades." Perhaps that should be amended to mention something about possibly uncontrolled satellites and space stations ![]() Dale |
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On Sun, 19 Mar 2006 13:55:38 +1100, "BlagooBlanaa"
wrote: Considering the number of research satellites that fail or partially fail due to instrument or other presumably fixable problem, why aren't satellites (whose mission profiles permit) launched to a near enough vicinity of the ISS so that astronouts can go out and fix 'em Because different satellites need to be in different orbits. Observation satellites are in orbits that pass over (or nearly over) the poles, so that they overfly all of the Earth's surface over a given period of time as the Earth rotates beneath the orbit. They also like to be down low to get as sharp a view as possible. But down low, you need a lot of fuel to counteract the drag of the tenuous upper atmosphere, so if you don't have to be down that low, you don't want to be. Meanwhile, most relay satellites need to be perfectly aligned with the equator and way up high, where one orbit of the Earth takes 24 hours and the satellite appears to be stationary in the sky, which in turn makes pointing antenna on the ground easier. But it takes a larger rocket and a more fuel to get a satellite up to that altitude and change its inclination to match the equator. And for satellites where the exact orbit is not critical, such as some astronomy missions, the sponsoring agency tends to choose the most efficient orbit its rocket can reach. For NASA, that's a 28.5 degree inclination orbit due east out of Cape Canaveral. For Russia, its a 51 degree orbit more or less due east out of Baikonour. Due east launches take most advantage of Earth's rotational velocity, meaning a heavier satellite can be launched on a given rocket, or a smaller, cheaper rocket can be used. That results in satellites being launched in numerous, incompatible orbits. Building one Space Station that can service all orbits is more or less impossible. Brian |
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Thanks for the replies
they don't hold water though, heres why 1) ISS to be moved via electromagnetic tether (google it) 2) Different orbits, schmorbits - what dictates energetics of mission parameters? If sats are assembled on orbit then you don't need to worry about this so much 3) Geosynchronous IS a different matter, hence I posited that it may be a good enough reason to have Geosynchronous habitats 4) ISS is resupplied via Russian cargo rockets... So not scared of misses, hmmmm? also payloads could be sent to rendezvous with tether, then to on-orbit assembly 5) ISS is stupidly expensive, not all habitats/factories have to be so. such a system of orbital habitats/factories/sat service stations can easily pay for itself |
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On Mon, 20 Mar 2006 10:06:30 +1100, "BlagooBlanaa"
wrote: Thanks for the replies they don't hold water though, heres why 1) ISS to be moved via electromagnetic tether (google it) Then it can no longer be supplied or crewed by the Russians. They're stuck launching to 51.6 deg. orbits. Any do you might have noticed, no one else is supplying or crewing ISS lately. 2) Different orbits, schmorbits - what dictates energetics of mission parameters? Objective of the mission, of course. You still can't expect the same results from an Earth Observation satellite at 28.5 degrees just because that's where the Orbital MRO Depot is. If sats are assembled on orbit then you don't need to worry about this so much Yes, you do. Where they're built has little impact on where they're going. (No one builds satellites at Kourou.) 3) Geosynchronous IS a different matter, hence I posited that it may be a good enough reason to have Geosynchronous habitats Better to have a Maneuvering Vehicle that can go up there and get them. You don't want to be sending crews back and forth through the van Allen belts willy nilly. 4) ISS is resupplied via Russian cargo rockets... Which can get no lower than 51.6 deg. inclination. (why ISS is there instead of the Shuttle's optimal 28.5 deg orbit.) 5) ISS is stupidly expensive, not all habitats/factories have to be so. True, but to handle satellite servicing, ISS is probably close to the size you'll need. Fewer lab modules, but more spare parts and tool depots and at least two servicing hangars. Probably need more people, too. In the end, the Orbital MRO Depot is going to be a beast. Brian |
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