Abstract. Schlieren imaging is a method used to visualize differences in refractive index within a medium. It is a powerful and straightforward tool for sensitive and high-resolution visualization of, e.g., gas flows.Here, heated cold gas microthrusters were studied with this technique. The thrusters are manufactured using microelectromechanical systems technology, and measure 22×22×0.85 mm. The nozzles are approximately 20 µm wide at the throat, and 350 µm wide at the exit. Through these studies, verification of the functionality of the thrusters, and direct visualization and of the thruster exhausts was possible. At atmospheric pressure, slipping of the exhaust was observed, due to severe overexpansion of the nozzle. In vacuum (3 kPa), the exhaust was imaged while feed pressure was varied from 100 to 450 kPa. The nozzle was overexpanded, and the flow was seen to be supersonic. The shock cell period was linearly dependent on feed pressure, ranging from 320 to 610 µm. With activated heaters, the shock cell separation increased. The effect of the heaters was more prominent at low feed pressure, and an increase in specific impulse of 20% was calculated. It was also shown that schlieren imaging can be used to detect leaks, making it a valuable, safe, and noninvasive aid in quality control of the thrusters.