Minty said:
pervect: thanks for the link, interesting reading. The fuel issue is discussed in terms of conservation of energy and momentum resulting in large fuel to weight ratios that probably correspond to the views expressed elsewhere; that the amount of fuel required (even at 100% mass conversion) quickly becomes unmanagable.
I'm a bit suspicious, though, that the calculations are all undertaken from the normal space frame of reference rather than the ships frame of reference.
The suggestion that the fuel be hydrogen scooped from interstellar space would appear to have merit in this context as the fuel is not part of the mass equation.
The calculations should all be in the ships frame of reference AFAIK.
The fuel usage part of the equation is easy enough to derive. The best case is a "photon drive", when the exhaust is light. The most logical almost-candidate for such a drive is the beam-core antimatter rocket
http://www.islandone.org/APC/Antimatter/02.html
but note that since this (hypothetical) design exhausts pions rather than photons, the performance will be worse in terms of mass ratio than the photon drive equations that I'll derive below.
If we use units such that c=1, we can say that with a photon drive, the exhaust energy E will be the exhaust momentum P as E = Pc, and c=1. Thus:
dp/dt = m*a = -dm/dt
where a is the proper acceleration of the ship, and dm/dt is the rate of change of mass of the ship. (Note that since c=1, mc^2 = m, so the rate of change of the mass of the ship is the same as the rate of change as its energy).
Thus a*dt = -dm/m, or ln(m) = -a*t+C, where C is some constant.
If we let m0 be the initial, fuelly fuelled mass of the ship, we can then say
m(t) = m0*exp(-a*t), where a is the proper acceleration (i.e. acceleration as measured from the ship), and t is the proper time (i.e. time as measured by the ships clock). Or if we let mf be the final (dry) mass of the ship, we can write
mass ratio = m0/mf = exp(a*t)
Since 1g is about 1 light year/year^2, we can see that we are talking about mass ratios of exp(20) or so to accelerate at 1g for 20 years even with a 100% efficient photon drive.
Another "downer" is that almost any conceivable design for a photon drive or a beam core antimatter rocket will probably melt itself into a puddle of slag long before it could reach a 1 g acceleration. If a rocket had a fueled mass of 10,000 metric tons, it would require that one convert .3 kg /second of matter to energy per second and exhaust it out the back. That's about 6 megatons/second. The beam-core design is one of the more theoretically efficient antimater drives, but it is expected to be no more than 60% efficient (because about 1/3 of the generated pions will be uncharged and will spread in all directions). That leaves a couple of megatons/second to be dissipated by a fairly small ship.
But these practical issues can be ignored for fictional purposes.
The ramjet proposal, BTW, is a possible source of additional mass for the ship, as you point out, but it has drawbacks. Remeber that the interstellar medium is coming in towards you at hyper-relativistic velocities, and when gamma >> 1, most of the incoming energy will be due to the velocity of the interstellar hydrogen, only a small fraction of it (the energy flux) will be due to the rest mass of the hydrogen.
You'll probably have to sweep it out of the way to avoid being thorougly fried but it'll be hard to turn a "net profit" in terms of the rocket's energy budget.