The combustion of hydrogen and oxygen is commonly used to power rocket
engines:
2H2 (g)...
Chemistry, 10.04.2020 18:39 officialrogerfp3gf2s
The combustion of hydrogen and oxygen is commonly used to power rocket
engines:
2H2 (g) + O2 (g) → 2H20 (g)
If the final pressure of water vapor was 0.875 atm and the temperature is 400. K,
how many mols of H20 was produced assuming that the reaction went to
completion in a 250. L engine?
mols
Round your answer to three significant figures. Do not include units in your answer.
Enter the answer
Answers: 2
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