For Project Hephaestus, a pintle injector was chosen due to its sufficient efficiency, machinability, and ability to mitigate combustion instabilities.
One of the main challenges with using a pintle injector for a nitrous-ethanol combo is spray angle. A lower spray angle is desirable because it means the mixed propellant has to travel further to reach the wall, and so can disperse more. However, when using nitrous-ethanol as propellants, a high mixture ratio is often used. This means that the nitrous will have a lot more momentum than the ethanol, and since the pintle is ox-centered (there is basically no way to manifold the regen cooling to the center of the injector to have it be fuel centered) the spray angle will be exceedingly high. However, we intend on drilling the pintle holes at an angle to enforce a lower spray angle.
This is the first iteration of the pintle injector, with some dimensions (i.e. number of film cooling holes or number of radial bolts not calculated yet). Also, holes at the bottom are not added yet. However, the final design will most likely closely resemble this, as it is machinable and contains no interpropellant seals.
The pintle center body/tip is made out of copper, while the baseplate is made out of steel. The interruption in the manifold is so igniter/PT ports can connect to the chamber offset from the holes. As of now, this injector stiffness is still (barely) above 15% for 25% throttle. However, we haven't accounted for pressure loss in the regen channels yet. However, since the fuel and oxidizer will be in separate tanks, the fuel pressure is not reliant on the ox pressure; we can increase the tank fuel pressure to account for the
Future things to consider: