One of my goals for 2023 is to design, build, test, and fly a liquid bi-prop rocket motor. I’m NAR level 3 certified and a member of both DARS and TNT (Tripoli North Texas) which are some local high power rocketry clubs. A friend of mine close with the TNT leadership has said getting permission to use their Seymour TX launch site for testing a liquid biprop motor may not be completely out of the question.
My design is based off the work done by the guys at halfcatrocketry.com, specifically their piston approach to fuel side pressurization. My tank is a 54mm hybrid rocket motor tank from Contrails Rockets and i plan to use a nitrous/methanol+nitro (basically rc engine fuel) oxy/fuel combination which has been proven by halfcatrocketry.com.
My plan is to target the J-K impulse range and fly the engine in a basic 4" (body tube width) airframe. I have the tank, valves, and a quick-disconnect remote fill arm built and on a test stand. Remote fill is handled through a pi zerow running a webapp and some python controlling servos used for fueling and disconnect. All my work so far has involved mostly OTS components from Contrails Rockets and 3d printing. The next test on-deck is a full pressurization test of the tank and valves (this is like “cryo testing” in the real deal rockets). The next major component to be produced is the combustion chamber.
Here’s the rub, I can model and design a combustion chamber but it’s not something you can just buy (or easily 3dprint), it has to be machined. I am not a machinist and want to learn how to use the machine shop but it’s going to take time. The machine shop and other amazing facilities and people of the makerspace is why I’m here. However, time is the one resource I can’t predict, i have a family and very demanding day job my ability to physically get to the makerspace will fluctuates wildly.
many hands make for light work, anyone interested?