At an elevation of 10 km above sea level (about 33,000 feet, approximately the cruising altitude of a jet airliner), the atmospheric pressure is 210 Torr and the temperature is 230K. Assuming air is 21% O₂, how many L of air at this altitude would be required to completely burn 1 kg of jet fuel, C₁₂H₂₆?

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The Answer of At an elevation of 10 km above sea level (about 33,000 feet, approximately the cruising altitude of a jet airliner), the atmospheric pressure is 210 Torr and the temperature is 230K. Assuming air is 21% O₂, how many L of air at this altitude would be required to completely burn 1 kg of jet fuel, C₁₂H₂₆?

At an Elevation of 10 Km Above Sea Level (About