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Colony ship propulsion
Hello. I've identified a huge problem in my novel and would appreciate any help.
Short version:
How much mass can you safely move, given 100-200 years travel time, to a nearby star system using the world's nuclear stockpile for pulse propulsion? This would be from Earth orbit to insertion around a similar planet.
Long version:
I'm on the second manuscript of a sci-fi series, which assumes the premise of a virtual multiverse. As such the systems programmers will offer 21st century humanity limited black-box technology: One aspect of the novel is how to marshal proven and theoretical technology, not wave a magic wand. The planet Gaia (in a parallel universe) is doomed and we have a scant sixty years to build a colony ship/biosphere. One of many problems: How to accelerate a large vessel out of the solar system and to a new planet, say 10-15 ly away within a century or two.
The ship is a modified Stanford torus, with counter-rotating "wheels" and a cylindrical hub from which we can provide our main thrust. The wheels are segmented so each biosphere can pivot during acceleration/deceleration. It will be assembled in orbit: We are giving doomed humanity all the launch capability it needs, via space elevators and whatnot. According to my research, anti-matter is too problematic to even consider for rocket fuel. But since we're not worried about leaving a trail of radiation behind, it seems that the best method is off-the-shelf nuclear pulse propulsion, a la Orion:
http://en.wikipedia.org/wiki/Project_Orion_(nuclear_propulsion) and http://en.wikipedia.org/wiki/Spacecraft_propulsion
Let's assume we have 1975's world nuclear weapons stockpile to play with (about 25,000 megatons yield). Dyson's figures show 280 kt total yield used to push about 10,000 tons of mass for interplanetary travel. Does this scale up to mean that 25,000 mt of yield will accelerate/decelerate 2.7 trillion tons to a nearby solar system? Naturally we would use the large area of the aft ring to spread a solar sail for start/finish of the trip. Other helps: whatever makes sense for ion thrusters around our rings; gravity assists where possible; launching fuel supplies in advance to be retrieved along the way; scaling the ship down (tugboat instead of a cruise ship).
Finally, if it would be possible to build, the ship I came up with has four rings with a total volume of approx. 1,400 cubic miles. Let's say for calculation purposes it contains 10% water and 90% air (1 atmosphere). I come up with 654 billion standard tons. We give ourselves lightweight nano-materials in the structure, hub, spokes and machinery. Add people, flora, fauna, supplies, fuel, etc., and round up to 1.5 trillion tons (1,360 trillion kg).
Throw in gobs of brilliant engineering, impeccable programming, laser weapons for space junk, load the nukes and light the fuse. What'd I miss?
Thanks in advance.
Hello. I've identified a huge problem in my novel and would appreciate any help.
Short version:
How much mass can you safely move, given 100-200 years travel time, to a nearby star system using the world's nuclear stockpile for pulse propulsion? This would be from Earth orbit to insertion around a similar planet.
Long version:
I'm on the second manuscript of a sci-fi series, which assumes the premise of a virtual multiverse. As such the systems programmers will offer 21st century humanity limited black-box technology: One aspect of the novel is how to marshal proven and theoretical technology, not wave a magic wand. The planet Gaia (in a parallel universe) is doomed and we have a scant sixty years to build a colony ship/biosphere. One of many problems: How to accelerate a large vessel out of the solar system and to a new planet, say 10-15 ly away within a century or two.
The ship is a modified Stanford torus, with counter-rotating "wheels" and a cylindrical hub from which we can provide our main thrust. The wheels are segmented so each biosphere can pivot during acceleration/deceleration. It will be assembled in orbit: We are giving doomed humanity all the launch capability it needs, via space elevators and whatnot. According to my research, anti-matter is too problematic to even consider for rocket fuel. But since we're not worried about leaving a trail of radiation behind, it seems that the best method is off-the-shelf nuclear pulse propulsion, a la Orion:
http://en.wikipedia.org/wiki/Project_Orion_(nuclear_propulsion) and http://en.wikipedia.org/wiki/Spacecraft_propulsion
Let's assume we have 1975's world nuclear weapons stockpile to play with (about 25,000 megatons yield). Dyson's figures show 280 kt total yield used to push about 10,000 tons of mass for interplanetary travel. Does this scale up to mean that 25,000 mt of yield will accelerate/decelerate 2.7 trillion tons to a nearby solar system? Naturally we would use the large area of the aft ring to spread a solar sail for start/finish of the trip. Other helps: whatever makes sense for ion thrusters around our rings; gravity assists where possible; launching fuel supplies in advance to be retrieved along the way; scaling the ship down (tugboat instead of a cruise ship).
Finally, if it would be possible to build, the ship I came up with has four rings with a total volume of approx. 1,400 cubic miles. Let's say for calculation purposes it contains 10% water and 90% air (1 atmosphere). I come up with 654 billion standard tons. We give ourselves lightweight nano-materials in the structure, hub, spokes and machinery. Add people, flora, fauna, supplies, fuel, etc., and round up to 1.5 trillion tons (1,360 trillion kg).
Throw in gobs of brilliant engineering, impeccable programming, laser weapons for space junk, load the nukes and light the fuse. What'd I miss?
Thanks in advance.
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