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Saw a documentary on Project Orion a couple of nights ago and it got me thinking about different methods of rocket propulsion, specifically over distances longer than our solar system - figured I'd start another physicsy thread.
Here's the two most interesting methods that I know of:
http://en.wikipedia.org/wiki/Bussard_ramjet
And a slightly more 50's solution, although I agree with Carl Sagan that it's a very practical way of decommissioning all those unnecessary nuclear weapons
:
Project Orion (nuclear propulsion) - Wikipedia, the free encyclopedia
Discuss.
Disclaimer: This is a thread for the joys of scientific discussion, spacefaring and lulz. Anyone preaching or engaging in my-theory-is-better-than-your-theory member-waving competitions will be forcibly ejected from the thread in a barrage of scorn and off-topic reports. Kthx.
Here's the two most interesting methods that I know of:
http://en.wikipedia.org/wiki/Bussard_ramjet
from wiki said:Bussard proposed a ramjet variant of a fusion rocket capable of fast interstellar spaceflight, using enormous electro-magnetic fields (ranging from kilometers to many thousands of kilometers in diameter) as a ram scoop to collect and compress hydrogen from the interstellar medium. High speed forces the reactive mass into a progressively constricted magnetic field, compressing it until thermonuclear fusion occurs. The magnetic field then directs the energy as rocket exhaust opposite to the intended direction of travel, thereby accelerating the vessel.
And a slightly more 50's solution, although I agree with Carl Sagan that it's a very practical way of decommissioning all those unnecessary nuclear weapons
:Project Orion (nuclear propulsion) - Wikipedia, the free encyclopedia
from wiki said:Project Orion was the first engineering design study of a spacecraft powered by nuclear pulse propulsion, an idea proposed first by Stanisław Ulam during 1947. The project, initiated in 1958, envisioned the explosion of atomic bombs behind the craft and was led by Ted Taylor at General Atomics and physicist Freeman Dyson, who at Taylor's request took a year away from the Institute for Advanced Study in Princeton to work on the project.
By using energetic nuclear power, the Orion concept offered high thrust and specific impulse at the same time; the optimum combination for spacecraft propulsion. As a qualitative comparison, traditional chemical rockets (the Moon-class Saturn V or the Space Shuttle being prime examples) provide (rather) high thrust, but low specific impulse, whereas ion engines do the opposite. Orion would have offered performance greater than the most advanced conventional or nuclear rocket engines now being studied. Cheap interplanetary travel was the goal of the Orion Project. Its supporters felt that it had potential for space travel, but it lost political approval because of concerns with fallout from its propulsion. The Partial Test Ban Treaty of 1963 is generally acknowledged to have ended the project.
Discuss.
Disclaimer: This is a thread for the joys of scientific discussion, spacefaring and lulz. Anyone preaching or engaging in my-theory-is-better-than-your-theory member-waving competitions will be forcibly ejected from the thread in a barrage of scorn and off-topic reports. Kthx.
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