Physical or inert fire suppressants such as N2, Ar, and CO2 have been broadly used on earth, while CO2 suppressant is now employed aboard human-crew spacecrafts where the atmospheric environment is characterized primarily by low-velocity oxidizer flow. Effects of inert diluent gases (N2, Ar, He, CO2) on flame spread and extinction behavior over thermally-thick solid fuel with low-velocity opposed oxidizer flow environment were studied by experiments and numerical simulation. With the same oxygen volume concentration and flow velocity, the flame propagates fastest when He is used as the diluted gas, while propagates slowest in O2/CO2 environment. Further study found that CO2, which has a large heat capacity to decrease the flame temperature, reduces the flame spread through thermal effect, while He promotes flame spread rate through both thermal and transport effect. In O2/He environment, the flame extinction behavior is dominated by the diffusion effect through the greatest thermal diffusion to increase the excessive radiative heat loss ratio. In O2/CO2, the oxygen concentration limit comes second, which is dominated by thermal effect. The flammability range is the largest in O2/Ar. The simulation results show that in low-velocity flow environment, if the inert-gases can emit or absorb thermal radiation, the characteristic heat transfer length increases. However, the reabsorption of emitted radiation has small effects on flame spread. This study provides valuable data on flame dynamics in diluted gases and can help develop more effective and applicable fire extinguishing agent for manned spacecraft in microgravity.
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