Now denotes the instantaneous rest mass of the rocket, including its fuel and stored internal energy, and is measured in a fixed inertial frame. Assume the exhaust is expelled backwards with speed in the rocket's instantaneous rest frame. By the relativistic velocity-addition formula, material emitted at time has inertial velocity
It coasts at this velocity after emission.
The crucial change is that the expelled material's rest mass is not simply : some of the rocket's rest energy becomes exhaust motion. Instead, use conservation of relativistic energy. Put , so the rocket's energy is . The exhaust emitted during carries energy . For material moving at velocity , the relativistic energy-momentum relation gives momentum , since and . Hence the modified total momentum is
Meanwhile the total relativistic energy is . These expressions consistently account for both energy and momentum of the expelled material.
Differentiate the momentum formula. The momentum conservation law gives
To simplify it, use
Multiplying by , the equation becomes
The two terms containing cancel. Dividing by proves the relativistic rocket equation
For fixed finite velocities, the nonrelativistic limit gives . Hence the relativistic rocket equation reduces to
which is the nonrelativistic rocket equation.
The conserved quantities called energy in the two calculations include different contributions. The nonrelativistic calculation considered only kinetic energy, which increases as fuel releases internal energy; total energy including that internal reservoir is still conserved. Relativistic energy includes rest energy, and therefore includes the fuel's stored internal energy through the rocket's rest mass. That rest mass decreases as energy is transferred into the exhaust. Thus conservation of relativistic energy and the nonconservation of kinetic energy express the same physical conversion.