Liquid oxygen and liquid methane
We want to know whether a liquid methane spray can keep a rotating detonation going. Methane is also what a lot of newer upper stages burn.
Our first engine: a water-cooled rotating detonation combustor for liquid oxygen and liquid methane, in the 2 kN class. The first firing has to show the wave holding for five seconds after the igniter is off.
The engine design is in review as we talk to manufacturing partners and prepare for testing.
Conceptual section. Proportions and passages are simplified.
Feeds liquid oxygen and liquid methane into the channel.
A stiff injector: about two-thirds of chamber pressure or more across the plate, at about 271 psia. The finished injector is flow-tested to set its operating pressures.
The ring the detonation runs around, between the outer wall and the centerbody.
85 mm outer diameter, 5 mm gap.
Deionised water will cool both walls, from a supply we are building ourselves, for the whole firing of about seven seconds.
Printed copper-alloy bodies with internal cooling passages.
An annular throat and centerbody plug guide the exhaust out of the engine.
The geometry is under design review.
Starts combustion so we can study whether the wave keeps going on its own.
A hydrogen and oxygen torch through the chamber wall, to be proved on a bench first.
Build the electronics for pressure transducers and data acquisition, and help capture high-speed footage of the engine.
High-speed imaging, with thrust and operating-pressure measurements.
These are the choices for the first engine.
We want to know whether a liquid methane spray can keep a rotating detonation going. Methane is also what a lot of newer upper stages burn.
The combustor is the experiment, so the tanks and lines should stay simple.
A compact engine sized for development and testing on a university test stand.
Internal cooling channels carry heat away from both walls during firing.
We will test the igniter on a bench before integrating it with the engine.
Success is the first two. Performance is recorded on every firing but is not a pass mark.
| Result | What it means | How we check |
|---|---|---|
| Show the wave | The detonation keeps going around the channel for at least five seconds after the igniter is off. | High-speed imaging of visible wave behavior. |
| Fire again | The hardware comes out of the whole firing, about seven seconds from start to shutdown, ready to fire again. | Water cooling on both walls, and an inspection of the hardware after every run. |
| Record performance | Thrust, propellant flow and chamber pressure are recorded on every firing. They are data, not a pass mark. | Calibrated thrust stand, propellant flow metering and chamber pressure. |
Each step checks one thing before we start the next.
Finish the first design and get someone else to review the numbers before we build anything.
In progressMachine or print the copper hot section and CT-scan the cooling channels.
NextRun water and stand-in fluids, then check the valves, sensors, and abort.
PlannedFire the engine, write down the measurements, and inspect the hardware afterward.
PlannedWe are looking for students who want to own a part of the engine, and for partners who can help us build and measure it. If you want to join or have any questions, just email us.