Experimental results obtained on a 600-kJ Electrothermal Launcher are
presented, Parametric studies have been completed at the energy level
of 150 kJ for analyzing physical processes. The optimal working fluid
mass has been determined by efficiency measurements and correlated wit
h a calculated value. The gas expansion has been studied by varying pr
ojectile masses and by a time-resolved pressure and velocity measureme
nt, These results allowed us to determine the polytropic exponent of t
he plasma,