THERMAL, CHEMICAL, AND RHEOLOGICAL ANALYSIS OF LUNAR HIGHLAND SIMULANTS
Two lunar highland simulants, NU-LHT-5M HQ and CSM-LHT-1G, were characterized using X-ray fluorescence spectroscopy, pycnometry, calorimetry, viscometry, and light flash analysis. NU-LHT-5M HQ is the glass component of a NASA simulant under development, and CSM-LHT-1G is a partially crystalline simulant made of several components. Their densities are similar in both glass and powder forms, in the range 2700-2800 kgm-3. Heating at 30 Kmin-1, NU-LHT-5M had a glass transition (Tg) at 788°C and reached liquidus (Tliq) at 1459°C. Powdered CSM-LHT-1G reached Tg at 616°C and Tliq at 1534°C. Remelted glass CSM-LHT-1G reached Tg at 750°C and Tliq at 1425°C. Total enthalpy required to heat NU-LHT-5M HQ glass to 1600°C was ~1681 Jg-1K-1 and for CSM-LHT-1G powder it was ~2275 Jg-1K-1. At 1600˚C, the viscosity of molten NU-LHT-5M HQ was 1.9 Pa·s, and for CSM-LHT-1G it was 2.6 Pa·s. Thermal diffusivity of NU-LHT-5M glass was 0.55mm2s-1 at 25°C and 0.52mm2s-1 at 600°C, and thermal diffusivity of CSM-LHT-1G was 0.54mm2s-1 at 25°C and 0.52mm2s-1 at 600°C. Thermal conductivity of NU-LHT-5M HQ glass was 1.225 Wm-1K-1 at 25°C and 1.472 Wm-1K-1 at 600°C. Thermal conductivity of CSM-LHT-1G was 1.200 Wm-1K-1 at 25°C and 1.434 Wm-1K-1 at 600°C.
These results reveal that once molten, the two simulants behave quite similarly despite their different chemical compositions. This suggests that moderate variation of the highland regolith material will not significantly impact the performance and the design of the equipment that may be used to process them.