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| Hypographer ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() | Re: Mission to Neptune Quote:
---------------- Your Friendly Neighborhood AdministratorWant to sponsor Hypography? Buy a print in our Fall 2008 Benefit Sale Join our Facebook group or follow us on Twitter Science is not only compatible with spirituality; it is a profound source of spirituality. - Carl Sagan | ||
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| Understanding | Re: Mission to Neptune Quote:
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You are not comparing like with like. Casini used radioisotope thermoelectric generators. These were a good choice for powering the instruments - given that solar power was not a viable alternative at the time. The demand was for 600-700 watts. While RTG's are viable for powering instruments it is not suggested that they are valid for powering ion drives. The power requirement for the JIMO is pencilled in at about 100,000 watts. Current RTG's would be far too heavy for such a task. If nuclear power is to be used for ion drives, it will be a totally new technology. The plans are for a fission powered generator. There is a real difference. Cassini used 3 RTG's, and if more power had been needed more RTG's could have been added. If a RTG had failed, it would be no great problem - there is redundancy. For the JIMO project there will be and can only be one fusion power source. One huge source of heat that must be dissipated. It is heat dissipation that will be the problem. Presumably there will be a large array of delicate cooling fins connected by heat pipes. I would like you to consider the development and deployment of this array. Can it be launched as a unit? If not, can it be assembled in space? How can it be made reliable? Leaks due to meteorite damage, mechanical stress during launch, thermal stress during operation, or radiation damage are all possible. So are blockages. There is plenty of information on ion drive development, and it's all going well. There is plenty of information on lightweight fission generators for space, and again it seems no great problem. Plenty of studies have been made. But for cooling - Where are the contracts for research and development? Where are the estimates of the cooling assembly's weight? All I have seen is an artists impression of what the cooling fins will look like. Quote:
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| Understanding | Re: Mission to Neptune Quote:
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| Hypographer ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() | Re: Mission to Neptune Blame, I think your posts here are very good. Thanks. ---------------- Your Friendly Neighborhood AdministratorWant to sponsor Hypography? Buy a print in our Fall 2008 Benefit Sale Join our Facebook group or follow us on Twitter Science is not only compatible with spirituality; it is a profound source of spirituality. - Carl Sagan | |
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| Understanding | Re: Mission to Neptune Quote:
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| Understanding | Re: Mission to Neptune Quote:
It would be no new thing for NASA to pay private companies for research. Nor will it surprise me that private industry has made useful developments that can be applied to space. Always we take what we already know and then using it as a base for development. Are you suggesting that private industry IS directly funding development of fusion power specifically for space? I doubt it. NASA will have to pay the vast bulk of any project to adapt our knowledge of earth bound reactors for application in space. | ||
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| Understanding | Re: Mission to Neptune Quote:
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