Surface temperature measurements on ablation models are described that demonstrate the application of photographic pyrometry to arcjet, arc tunnel, and rocket exhaust facilities. Sharp temperature discontinuities and hot spots are shown to be a predominant characteristic of the ablative surfaces tested, increasing the importance of spatial temperature measurements. The photographic pyrometry technique is, therefore, extremely valuable for determining point temperatures on the rough temperature contours, whether produced naturally as a result of the ablation process or by immersion sensors of vastly different thermal properties than the ablation material. The restrictions placed on the optical measurements by extraneous radiation are discussed and, in general, are found to be minor. An accuracy of 2-3% is estimated for these tests in the temperature range 1250-3800°K encompassing a possible inaccuracy of approximately ±14% in the mean emittance estimate of 0.88 for the ablators.