The gasdynamic mirror (GDM) plasma thruster has the ability to confine high-density plasma for the length of time required to heat it to the temperatures corresponding to specific impulse requirements. The often-cited plasma confinement time is directly proportional to the mirror ratio and the length, and is inversely proportional to the square root of ion energy. This confinement law, however, ignores the role of the ambipolar (electrostatic) potential which arises as a result of the rapid escape of electrons through the mirrors due to their small mass. This positive potential tends to accelerate the ions while slowing down the electrons until both species drift out at the same rate. It is expected, therefore, that a larger specific impulse and larger thrust will arise in the presence of ambipolar potential but at the expense of a longer device to maintain a desired confinement time. This proposal is aimed at a theoretical and computational investigation of the impact of the ambipolar potential on the propulsive capability of the GDM thruster. It includes the generation of parameters that will allow experimental verification of this phenomenon using the existing GDM device at the Marshall Space Flight Center (MSFC).