Radiation-driven flame spread over thermally thick fuels in quiescent microgravity environments

Abstract

Microgravity experiments of flame spread over thermally thick fuels were conducterd using foam fuels to obtain low density and low thermal conductivity and thus large spread rate (Sf) compared to dense fuels such as polymethylmethacrylate. This scheme enabled meaningful results to be obtained even in 2.2 s drop tower experiments. It was found that, in contrast to conventional understanding, steady spread can occur over thick fuels in quiescent microgravity environments, especally whenm a radiatively active diluent gas such as CO2 is employed. This is proposed to be due to radiative transfer from the flame to the fel surface that can lead to steady spread even when conductive heat transfer from the flame to the fuel bed is negligible, Radiative effects are more significant under microgravity conditions because the flame thickness is larger and thus the volume of radiating combustion products is larger at microgravity. The effects of oxygen concentration and pressure are shown and the transition from thermally thick to thermally thin behavior with decreasing bed thickness is demonstrated. A simple semiquantiative model of radiationdriven flame spread rates is consistent with experimental observations. Radiative flux measurements confirm the proposed effects of diluent type and gravity level. These results are particularly noteworth considering that the International Space Station employs CO2 fire extinguishers; our results suggest that helium may be a better inerting agent on both mass and mole bases at microgravity even though CO2 is much better on a mole basis at earth gravity.