“…Historically, most IR-LAS sensing in scramjets has employed near-IR telecommunication-grade TDLs for measuring temperature, H 2 O, and velocity in continuous-flow facilities [291,178,43,293,124,188,296,297], with only one prior example of measuring CO 2 in [292] (later discussed in [41]). Recently, several efforts have extended sensing capabilities to: 1) the mid-infrared for improved measurements of H 2 O [184,294], CO 2 [219,294], and the first measurements of CO [219,294] in a hydrocarbon-fueled model scramjet combustor, 2) 2D via tomography [124,190,126], 3) greater bandwidth for improved sensing in impulse facilities [244,159], and 4) the first in-flight TDLAS measurements for characterizing scramjet flow fields [26,27,28,298].…”