Gell-Mann and Low theorem

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A photon rocket is a hypothetical rocket that uses thrust from emitted photons for its propulsion.[1] The standard textbook case of such a rocket is the ideal case where all of the fuel is converted to photons which are radiated in the same direction. In more realistic treatments, one takes into account that the beam of photons is not perfectly collimated, that not all of the fuel is converted to photons etc., see e.g. Nuclear photonic rocket.

Speed

The speed an ideal photon rocket will reach in the absence of external forces, depends on the ratio of its initial and final mass:

v=c(mimf)21(mimf)2+1

where mi is the initial mass and mf is the final mass.

The gamma factor corresponding to this speed has the simple expression:

γ=12(mimf+mfmi)

Derivation

We denote the four-momentum of the rocket at rest as Pi, the rocket after it has burned its fuel as Pf, and the four-momentum of the emitted photons as Pph. Conservation of four-momentum implies:

Pph=PiPf

squaring both sides (i.e. taking the Lorentz inner product of both sides with themselves) gives:

Pph2=Pi2+Pf22PiPf

According to the energy-momentum relation, the square of the four-momentum equals the square of the mass, and Pph2=0 because all the photons are moving in the same direction. Therefore the above equation can be written as:

0=mi2+mf22mimfγ

Solving for the gamma factor gives:

γ=12(mimf+mfmi)

References