Special relativity: What is the final mass of the rocket?

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SUMMARY

The discussion focuses on calculating the final mass of a rocket utilizing photon fuel while traveling at a speed of 0.5c. The initial energy is defined as M0c², equating to the final energy comprising both the energy of the photons and the final energy of the rocket, which incorporates the Lorentz factor gamma (γ). The participant expresses concern about the complexity of the equations and the number of variables involved, suggesting that a simpler kinematic approach using conservation of energy and momentum may yield the result more effectively.

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  • Understanding of special relativity concepts, particularly Lorentz transformations.
  • Familiarity with the conservation of energy and momentum principles.
  • Knowledge of photon energy calculations, including frequency and wavelength relationships.
  • Basic proficiency in algebraic manipulation of equations involving gamma (γ) factors.
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  • Study the derivation of Lorentz transformations in special relativity.
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  • Explore photon energy calculations, focusing on the relationship between frequency, wavelength, and energy.
  • Review conservation laws in relativistic contexts, particularly for systems involving variable mass.
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sabre729
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Homework Statement


Ok, the problem says some rocket of mass M0 has this new technology that allows it to convert photons into fuel. It reaches a speed of .5c. The problem asks us to solve for the final mass of the rocket, and then assume that all the lost mass was converted into photon fuel and calculate the total energy of that.


2. Attempt at a solution
Of course the starting E is just M0c^2 because it's starting from rest.

It's equal to the final energy: E(photons)+E(rocket, final).

The rocket's final mass is going to have some factor of gamma (γ) multiplied in, which in the case of .5c (β=.5) is equal to about 1.15. After factoring in the momentum of the rocket:

M0*c^2=E(initial)=E(final)=E(photon)+((γM0*c^2)^2+(γ*β*M0*c)^2)^(1/2)

First off, is this expression okay? Lorentz transform-wise it makes sense that the rocket's energy and momentum are multiplied by γ and γ*β, since we are looking at the speed in the rocket's frame and then boosting it back to the stationary frame. It also factors in the E(photons), which in this case is equal to n*H*v/c, where v is the frequency and c is the speed of light.

But doesn't this give me too many variables to express the change in mass? Unless the mass is only the part of the equation that doesn't include the photons (hence the "mass defect" goes to the photons).

Does what I did make sense to anyone who isn't me?
 
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That looks a little too complicated to me. You should be able to find the result by just doing the standard kinematic calculation with conservation of energy and 3-momentum. You can write the equations in terms of 4 variables: initial mass of the rocket, mass of the fuel converted, energy of the photons and gamma.
 

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