A mesa-scale heat recirculating thrust chamber has been developed for use with methanol, by utilizing steam/oxygen as an oxidizer. The steam/oxygen mixture serves as a surrogate for hydrogen peroxide. The extinction regimes, discharge characteristics, and both steady state and pulsing thrust characteristics are presented. Differences between the extinction behavior of the thrust chamber both without and with the nozzle were explored and a non-dimensional extinction criterion established to predict low Re extinction. The discharge characteristics: coefficient of discharge and characteristic velocity efficiency were determined and correlated to throat Reynolds number, Thrust measurements taken with the indirect method show reasonable agreement with the isentropic solution for the experimental stagnation conditions, suggesting high nozzle efficiency despite low chamber pressures and high gas temperatures. The behavior of the thrust chamber in pulsed configuration was tested with methanol/oxygen and methanol/water/oxygen mixtures. High speed cinematography was used to study the evolution of the flame during the pulse. (c) 2012 Elsevier Ltd. All rights reserved.