A pulsed arc heater was designed, manufactured, and installed in Centrospazio laboratory to equip a newly developed hypersonic, high-enthalpy, small-scale blowdown wind tunnel. The facility operates with air in the low to medium Reynolds number range (10 4 -10 6 ) and is capable of producing Mach 6 air ows, with a speci c total enthalpy up to 3 MJ/kg, on a 60-mm effective diameter test section. The heater is run in a pulsed, quasisteady mode, with test time ranging between 10 and 50 ms. The ow is directly heated by the electric arc established between two coaxial electrodes, powered by a large capacitor bank. A suitable plenum chamber placed just downstream of the discharge chamber allows the ow to reach thermochemical equilibrium before the expansion in the wind-tunnel nozzle and enhances mixing, thereby reducing radial gradients. A numerical model was developed to simulate the unsteady gasdynamic behavior of the arc heater and was used during the design phase to optimize the geometric and temporal parameters of the heater and to assess the hypersonic tunnel useful test time. Experimental results compare favorably with numerical predictions, with the plenum pressure history matching within 5% and plenum temperature within 10%. More than 600 runs have been performed so far, demonstrating the heater reliability and capabilities.