It's difficult to write this without sounding sarcastic, but I genuinely found this snippet very interesting. It's counter intuitive, but makes perfect sense.
Yes, it can be a little counter intuitive. Adding more oxygen drives up the temperature (until reaching a stoichiometric mixture), but that results in heavier products (e.g. CO
2 rather than CO). Exhaust gas velocity is proportional to (T/M)
1/2, so somewhere there is an optimum point that's hot enough and light enough to produce the maximum velocity.
I generally initially balance the combustion equation with enough oxygen such that all the carbon and hydrogen produce CO and H
2O. I'll then adjust the amount of oxygen up or down (usually down) until I find the optimum point. In the case of SiH
4, I kept adjusting down and down, and the exhaust velocity keep going up and up. I ended with less than half as much oxygen as I started with. All rockets run fuel-rich but this was extreme.
After reading these discussions I'm beginning to wish I took a different career path.
I don't have any regrets with the career I chose, but I definitely wonder sometimes how things would have worked out had I decided to go into aerospace instead.