| Thread | Last Post | Replies |
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| Earth-Jupiter fast transit | 31 Dec 2003 17:18 GMT | 2 |
I'm trying to figure out time-of flight for hyperbolic fast transits from Earth to Jupiter, and it's not going well. Can anybody point me towards either a table of such (with, say, varius departure V's at earth, and the time of flight to Jupiter orbit), or perhaps a
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| Lunar Sample Return via Tether | 31 Dec 2003 16:56 GMT | 38 |
My father (Henry Cate) and I have come up with an initial tether project that might be fun, affordable, and profitable. The idea is to use a rotating tether to pickup some Lunar samples, bring them back to Earth, and sell them.
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| Radiation a Mars trip hazard? | 31 Dec 2003 15:53 GMT | 15 |
http://www.nytimes.com/2003/12/09/science/space/09RADI.html The thing I don't understand is that people have been spending much more time in orbit than the round-trip to Mars. Although the upper atmosphere does shield them somewhat, the majority of the radiation is still getting
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| beagle failure guesses? | 31 Dec 2003 14:30 GMT | 4 |
I am holding out hope the mission will still succeed, but meanwhile, I'm trying to think of the possible reasons for failure, and what if anything could have been done to prevent or recover from them. Interested in your rankings of these possibilities or alternate most likely ...
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| Nexus Rocket Engine Test Successful; 10 Times More Thrust Than Deep Space 1 Engine and Lasts 3 Times Longer (10 years) | 30 Dec 2003 19:44 GMT | 5 |
Does anyone know how much this engine would cut down the time to a Mission to Mars. If such a mission could take 2 to 3 weeks then gentleman I'm convinced that we will have settlements on Mars in 10 to 15 years providing there is water up there.
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| HTHL vs VTVL - Wheeled sled for landing? | 25 Dec 2003 05:04 GMT | 3 |
Thinking about the problem some more it seems a big problem would be landing a high speed glider onto a sled that is on tracks. This would mean that the sled could only control it's movements in one dimension. A bad cross wind or gust leaves the glider to do all the working of ...
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| Improved Specific Impulse Rocket Engines | 24 Dec 2003 06:50 GMT | 6 |
Looking only at the vacuum specific impulse of plain hydrogen-oxygen rockets, is it possible to advance their specific impulse to 500, or even 520? For example, I recall Mr. Spencer recently mentioning that an ideal
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| Anniversary of sorts just past | 24 Dec 2003 04:49 GMT | 3 |
I had thought I remembered that the first posts in the then-brand-new sci.space reorg groups went out in early January 1994, but reviewing Google records found some from mid December 1993, one as early as
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| Artificial sunlight? | 23 Dec 2003 07:04 GMT | 3 |
In several experiments conducted by NASA and by the Russians plants were grown indoors using an artificial light. What type of light was used that produces light on the same wave lengths as the suns does? Christopher
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| RLV physicaly impossible ? | 22 Dec 2003 01:29 GMT | 14 |
I am really amazed by all these optimistic people trying to do rlvs and i belive in these peoples cause! however it strikes me that these people all seem a bit to optimistic for ex almoast all the groups i have investigated are into liquid propellant engines, and they seem to
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| Peroxide biprop ignition | 16 Dec 2003 03:11 GMT | 10 |
Some methods I've seen mentioned for peroxide biprop ignition are: Decompose the peroxide with catalyst pack. Pyrotechnic igniter in the chamber. Dissolve catalyst in fuel.
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| white knight: air-launched sst | 15 Dec 2003 23:23 GMT | 2 |
Would a supersonic jet the size of the spaceship-one gain much performance by being launched from underneath the white-knight from 48,000ft? Toby
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| Improved Isp Rocketry II | 15 Dec 2003 12:44 GMT | 3 |
Two questions this time: 1) Is it possible to get kerosene-LOX or propane-LOX to 395Isp? I've seen numbers around 360 on www.astronautix.com . 2) How effectively do large, altitude compensating nozzles
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| This is the most important CATS post ever! | 15 Dec 2003 11:59 GMT | 13 |
The technology described in this post has not been tested, but it looks trivial when compared to rocket launchers, and it may reduce the cost of space access to a few dollars per kilogram! The technology is based on GPS, a reusable sounding rocket,
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| Astrometry | 12 Dec 2003 22:01 GMT | 1 |
I understand that the large and expensive Gaia astrometry satellite will achieve very accurate stellar parallaxes from (I believe) the L2 point - which still only gives a 2AU baseline. Why not put a cheaper, lighter, less precise astrometry package on (say) Kuyper Express (or ...
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