With the prospect of using Al as fuel in a CO2 breathing engine in Mars atmosphere containing no oxygen, an experimental study on the ignition and combustion of Al was performed by using the stagnation region of impinging pure CO2 streams over a wide range of pressure and velocity of the streams. Al could ignite spontaneously in the CO2 streams, and the critical ignition temperature decreased with decreasing pressure and velocity of the streams. In the ignition process whether surface reactions proceeded initially to form a protective Al2O3 film on the Al surface or not was found to play a crucial role. When the surface was not covered with the film, ignition occurred in the gas phase leading to development of a luminous flame. During combustion, the Al surface remained clean, and AlO was produced in the gas phase due to the reaction of Al vapor with CO2. The AlO had a peak concentration in the gas phase away from the surface, and Al2O3 was condensed there. The burning rates of Al in the CO2 streams were estimated to be much lower than those of Mg in a CO2 stream and B in a O2 stream. The combustion mechanism for the Al-CO2 system has been postulated, including the surface and gas phase reactions producing Al vapor, AlO, Al2O, CO and condensed Al2O3. The ignition mechanism is discussed, and the role of CO2 diffusion from the upstream to the surface, controlled by a non-dimensional ejection parameter, is clarified.
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