Where can I find the formula for the relavistic rocket equation?

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SUMMARY

The discussion centers on the relativistic rocket equation, specifically the calculation of fuel mass required to accelerate a rocket from rest to a velocity β, given a specific acceleration A and an initial mass M. A reliable resource for this formula is provided, detailing both the classical and relativistic rocket equations. The classical equation is expressed as v_{class.} = p_{sp} \cdot ln(m_0/m), while the relativistic upgrade is given by v_{rel.} = v_{class.}/√(1 + v_{class.}^2/c^2). The specific impulse (p_{sp}) is also defined in terms of mass defect (d) and efficiency (η).

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  • Understanding of classical mechanics and rocket propulsion principles
  • Familiarity with relativistic physics concepts
  • Knowledge of specific impulse (p_{sp}) and its significance in rocketry
  • Basic mathematical skills for logarithmic and square root calculations
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  • Research the derivation of the relativistic rocket equation in detail
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Albertgauss
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Hi all,

Does anyone know where I can find the formula for the relavistic rocket equation? That is, I want to know the mass of fuel required to accelerate a rocket from 0 to β, for a given acceleration A, assuming the rocket (with no fuel) has a mass of M. All of this would be in the frame of the Earth. I know there are several types of proposed Sci-Fi fuels but I think fusion is the most promising. A reliable webpage would be great. Thanks!
 
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The classical rocket equation

v_{class.} = p_{sp} \cdot \ln \frac{{m_0 }}{m}

can be upgraded to a relativistic version by

v_{rel.} = \frac{{v_{class.} }}{{\sqrt {1 + \frac{{v_{class.}^2 }}{{c^2 }}} }}

and

p_{sp.} = c \cdot \sqrt {\left[ {2 + \left( {\eta - 2} \right) \cdot d} \right] \cdot \eta \cdot d}

where d is the mass defect and \eta the efficiency.
 
Oh hey guys great! Thanks! I think that will do it.
 

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