Acetone fluorescence provides a useful way to visualize the fluid mixing pr
ocess within supersonic wind tunnels, some of which operate in the low temp
erature (240-300 K) and low pressure range (0.1-1 atm). Measurements are pr
esented to quantify the dependence of the acetone laser induced fluorescenc
e (LIF) signal on temperature and pressure in this range. The temperature a
nd pressure sensitivity of the acetone LIF signal resulted in less than an
8% variation over the experimental conditions for a laser excitation wavele
ngth of 266 nm. Condensation of the acetone vapor was identified as a poten
tial problem for this diagnostic technique. Methods to prevent and check fo
r condensation are discussed.