“…For example, for jet engines used in fighter aircraft, the temperature is usually within the range of 800–1450 °C [ 4 ], and in volcanic research, lava usually exhibits a non-Newtonian flow state between 800 and 1120 °C [ 5 , 6 ]. Traditional pressure sensors are based on silicon or silicon-on-insulator technology, and cannot operate above 450 °C [ 7 , 8 , 9 ]. Pressure sensors based on SiC for application in harsh environments have been extensively developed, and a 4H–SiC piezoresistive pressure sensor has been reported which can operate up to 800 °C [ 10 , 11 , 12 , 13 , 14 ].…”