<?xml version="1.0"?>
<!--
  Turbo 550 at 8 V
  
  Data taken from
  Retzbach, Ludwig: Ratgeber Elektroflug, Neckar Verlag, 1991.

  M_r = 0.57E-2; // Nm
  I_0 = M_r/k_M = 1.43A
  
  J_M is just guessed.
  
  n_0 = 18605/min = 310/s



-->

<engine_dcm R_I="0.145" k_M="0.40E-2" I_0="1.43" J_M="1.0E-6">
</engine_dcm>
