Gaseous oxygen and ethanol hopper with a homemade electric pump

Oct 12, 2026 Last reply: 2 hours ago 4 Replies
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When everything runs, this hopper feeds itself: a DIY centrifugal electric pump pushes ethanol to a steel engine burning gaseous oxygen, with servo-actuated half-inch valves metering both fuel and oxidizer, and a gimbal rig swinging the nozzle to demonstrate thrust vector control. The whole point of the project is a rocket that lands itself, which is an ambitious target for a garage effort.



The construction details are what grab me. The maker printed the pump impeller in aluminum and 3D printed the engine in steel, cooled regeneratively by the fuel, so in theory it should be reusable. The engine carries two attachment points for the TVC arms. The airframe stands on four long metal tube legs joined by 3D-printed parts with flat foot pads, with a silver cylindrical tank up top and a black tank below on a wired frame. A vertical stack of six blue and white components sits on a white printed bracket, and red and blue fluid lines run to the engine with wiring routed along the structure. Design work was done in the free version of Fusion 360, and a 3D printer produced the PLA parts.



The propellant choices look sensible to me. Gaseous oxygen was picked as the easiest oxidizer to buy, and ethanol is easy to get and simpler to handle; the maker ruled out nitrous oxide over the hazards of a self-pressurizing liquid at -70 Celsius. Notably, the ethanol is not pre-pressurized, the pump alone does the feeding.



There are open items, as expected at this stage. No static fire has happened yet, so chamber pressure and specific impulse remain unmeasured; the targets are 6 bar and roughly 200 seconds. The pump has run on water, most recently without its enclosure, and a full test is still to come. The engine will first be fired fixed before the TVC arms are used, and whether it survives without exploding is honestly still an open question.


Curious about the pump side of this. The maker ran it with water in an early run and the last run happened without the enclosure fitted. Does anyone know what the full, completed pump test is planned to look like, and whether ethanol runs are scheduled before the engine is fired?

Running the chamber at a deliberately low pressure seems like a smart call to me. The pump is probably not that great, as the maker admits, and the low pressure also gives a good upstream pressure delta, hopefully avoiding explosions. Trading performance for that safety margin on a first liquid engine feels like the right kind of conservatism. The 200 second target still sounds respectable for this propellant combination.

I would love to see the TVC demonstration taken further once the fixed-engine burns are done. The gimbal lattice already shows a nice circular nozzle motion, and having two attachment points for the arms suggests a proper two-axis setup is possible. Swapping nitrous oxide in for a later version could also be worth revisiting, since the maker hinted maybe for the next project anyway.

On the thrust and nozzle question: the maker has said the engine first gets tested fixed, and only after that will the TVC arms be used. The nozzle sits in a 3D-printed lattice gimbal mechanism and moves in a circular motion to demonstrate the thrust vector control system. As for whether it survives without exploding, that has not been answered yet, since no static fire has been done and more testing comes first.

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