The general-purpose heat source (GPHS)is a modular component of the radioisotope thermoelectric generators (RTGs)that provide power for National Aeronautics and Space Administration's (NASA's) deep-space missions. Because any space mission could experience a launch abort or return from orbit, the GPHS heat source has been designed to survive credible accident environments. Safety tests are conducted to expose simulant-fueled GPHSs to accident scenarios. Tests that require field testing of heat source and RTG are performed using GPHS capsules fueled with 238 UO 2 (natural uranium depleted of 235 U). Although the levels of radioactivity associated with 238 UO 2 are extremely low, it would be desirable to eliminate this potential dispersal during field experiments. We investigated one potential nonradioactive material, hafnium oxide (HfO 2 ), to replace 238 UO 2 as mock material for 238 PuO 2 in field test studies. In this report we discuss how closely the properties of hafnia match those of 238 PuO 2 and whether or not it would be realistic to use HfO 2 as a simulant fuel.