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| Thorium Energy Amplifier | 30 Nov 2005 21:33 GMT | 2 |
Here's one I came across: http://www.reference.com/browse/wiki/Energy_amplifier A thorium fission reactor would be classified as an 'energy amplifier' because it cannot produce enough neutrons for a runaway reaction,
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| Space Fountain References | 24 Nov 2005 19:54 GMT | 2 |
I'm looking for citable references to the concept of a "fountain" or "dynamic compression member" concept for building towers to the edge space. The basic concept is that kinetic energy can be used to push the top of the tower up, similar to pushing a ping-pong ball up on a
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| Positronium as Hi-Energy Fuel | 24 Nov 2005 18:14 GMT | 3 |
We've already had discussions about anti-matter being used as a fuel one day, but typically there were criticisms about the stability of the magnetic bottles used to contain the anti-matter. Here is an article about positronium as a possible future power source:
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| Fast Fission Bombtrack to 45%c - 40year return mission | 19 Nov 2005 20:36 GMT | 1 |
Conventional wisdom is that fission can't produce fast interstellar velocities, except by powering a propulsion beam. Here, I show how bombtrack propulsion can be used to acheive 45%c. In particular, this propulsion method may be used to
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| what orbit maxes sunlight w/ ship that faces same way, i.e., due to rotating axis pointing at sun | 17 Nov 2005 18:50 GMT | 2 |
question: what orbit maxes sunlight w/ ship that faces same way, i.e., due to rotating axis pointing at sun - - - am trying to have large glassed area always facing sun while in LEO, to avoid any even small changes in sunlight due to not being sun-facing except for when in
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| An efficient orbit to fly a space craft from the L1 lagrange point to mars sun-synchronous orbit? | 10 Nov 2005 20:01 GMT | 2 |
Hello there everyone, I joined this competition callled The International Space Settlement Design Competition organized by Nasa. In the request for proposal of the
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| How are/were rockets stabilised | 08 Nov 2005 19:02 GMT | 7 |
With the source of thrust so far behind the centre of mass, large rockets would seem to be unstable in flight. So how is this overcome? I could imagine a sensitive gyro in the rockets nose, which enables a microprocessor to calculate the deviation from the planned line of
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| Jet engine 1st stage | 07 Nov 2005 17:50 GMT | 31 |
I am sure this topic has been covered here at some time but I missed it. Would it be feasible to use air breathing jet engines as the 1st stage (or as strap-ons) of a launch system? Of course, that is exactly what
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| Hydrogen to the Moon | 04 Nov 2005 20:28 GMT | 17 |
There's gobs of O2 on the Moon (~40% by mass of the Moon's surface is oxygen), but hydrogen is still needed to make water (remember, the poles are a long way from an economical-to-get-to equatorial Lunar base, so Lunar ice may not be a viable option in the short term) and also ...
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