SpaceCrazy5
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I've been researching a lot about rocketry, specifically rocket engines. I decided to give designing one a go, but I'm slightly stuck; how am I supposed to calculate the Specific Gas Constant of the combustion chamber gas?
It's mostly confusion to do with the molecular mass, and how that relates in terms of the oxidizer/fuel ratio, and other factors.
Sorry if I've posted this in the wrong place, I'm just confused!
It's mostly confusion to do with the molecular mass, and how that relates in terms of the oxidizer/fuel ratio, and other factors.
Sorry if I've posted this in the wrong place, I'm just confused!