This theoretical study derives the efficiency limit of self-field MPD thrusters, indicating critical performance factors.
A fundamental upper limit, η̂ , for the thrust efficiency of self-field magnetoplasmadynamic thrusters (MPDTs) is derived from the generalized Ohm’s law and the minimization of the volume integral of the square of the current density, which controls dissipation in the MPDT. It is found that η̂1/(1+4/R_mciξ⁴) , where ξ is the MPDT scaling number (the total current normalized by the current at which an equipartition of power occurs between thrust and ionization), and R_mci is the magnetic Reynolds number evaluated at ξ=1 .
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Edgar Choueiri (2026) studied this question.
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