# Output pressure of centrifugal pump

I'm trying to get my bearings (a somewhat heavy-handed expression) on pump design and I'm finding in the various books I've procured on the subject that there is very little consideration given to the output pressure developed by a pump.

If there isn't much detail to this question, I apologize; I'm still in the far-below-basic level of understanding. Obviously, head is a key parameter of pump design, but my concerns are with output pressure. The reason being, I'm considering for example rocket engine design where the key parameters of pump requirements are chamber pressure and flow rate. I understand that flow rate varies with head by the characteristic Q-H curves.

So, how does pump head vary with or affect the output pressure developed by a pump? Are the two concepts related, or are they independent of one another? If they are related, how would I go about figuring out the required head parameters from the pressure and flow requirements?

Head and pressure are effectively the same thing.

It's impossible to look at a pump and say "this pump will provide 10 bar of pressure." One of my favorite aspects of fluids has always been how interconnected an entire fluid system is, and how it stabilizes itself on its own. So the pressure that's actually supplied depends on the rest of the system: the losses in the pipe, the inlet and outlet conditions of the fluid to the system, the fluid itself, and how much power you're supplying to the pump.

$$P+{\rho}gz+{\frac12}{\rho}v^2=constant$$
(Remember that this can only be used for incompressible flows, but since we're talking about pumps and probably only common liquids at relatively low speeds, the incompressible assumption is fine. It only becomes an issue when $Mach>0.3$.)
$$\frac{P}{\rho g}+z+\frac{v^2}{2g}=constant$$
In this case, the constant has units of length (more specifically, units of length of a particular fluid, e.g. mmHg), and it's referred to as the head. But this term is fundamentally no different from the constant we get in the first equation, it's just expressed differently. $H=P_{total}/{\rho g}$, but because this is an imcompressible flow, the density is constant, and we know that $g$ won't change significantly unless we're moving the fluid over a massive height differential.