The formulas (for the acceleration phase) are:
time0 = c sinh(acc time / c) / acc
dist = c2 (cosh(acc time / c) -1 ) / acc
speed = c tanh(acc time / c)
mratio = exp(- acc time / exspeed)
where:
time0 = time relative to the Universe
acc = acceleration
time = time relative to rocket
dist = distance
speed = final speed
mratio = mass ratio
exspeed = exhaust speed
Page under construction. Suggestions or
requests are welcome
Created: 1998-05-04
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Contributors to this page:
- Sarah (s dot addams at telergy dot com)
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