Resonance Gen 1

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.

Design targets

Performance

Thrust
2 kN class1.55 to 1.82 kN expected
Chamber pressure
About 271 psiaDesign target
Mixture ratio (O/F)
3.00Nominal design point
Detonation hold
5 sAfter the igniter is off, within a firing of about 7 s

Geometry

Channel outer diameter
85 mmOuter bore diameter
Channel gap
5.0 mmRadial gap
Combustor length
51 mmInjector face to throat
Nozzle
Annular throatCenterbody plug

Systems

Propellants
LOX and LCH₄Pressure-fed
Total propellant flow
0.874 kg/s0.655 LOX, 0.218 LCH₄
Cooling
Deionised waterOuter wall and centerbody
Ignition
Gas torchHydrogen and oxygen, bench-tested first

Layout

The engine design is in review as we talk to manufacturing partners and prepare for testing.

Conceptual section of a water-cooled annular detonation engineAn injector and manifold feed a cylindrical annular combustion channel between two cooled walls. The centerbody widens near the annular throat, then tapers into a truncated plug outside the outer wall. A second view shows the ring-shaped channel. This illustration simplifies proportions and passages and contains no manufacturing dimensions.Longitudinal sectionExhaustAnnular cross-sectionCombustion channelWater coolingSectioned metal

Conceptual section. Proportions and passages are simplified.

  1. Preliminary

    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.

  2. Preliminary

    The ring the detonation runs around, between the outer wall and the centerbody.

    85 mm outer diameter, 5 mm gap.

  3. Preliminary

    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.

  4. Preliminary

    An annular throat and centerbody plug guide the exhaust out of the engine.

    The geometry is under design review.

  5. Set

    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.

  6. Preliminary

    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.

Design choices

These are the choices for the first engine.

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.

Pressure-fed

The combustor is the experiment, so the tanks and lines should stay simple.

2 kN class thrust

A compact engine sized for development and testing on a university test stand.

Water-cooled copper walls

Internal cooling channels carry heat away from both walls during firing.

Ignition testing

We will test the igniter on a bench before integrating it with the engine.

Goals for the first firing

Success is the first two. Performance is recorded on every firing but is not a pass mark.

ResultWhat it meansHow we check
Show the waveThe detonation keeps going around the channel for at least five seconds after the igniter is off.High-speed imaging of visible wave behavior.
Fire againThe 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 performanceThrust, 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.

Steps to the first firing

Each step checks one thing before we start the next.

  1. 1

    Design and review

    Finish the first design and get someone else to review the numbers before we build anything.

    In progress
  2. 2

    Build and inspect

    Machine or print the copper hot section and CT-scan the cooling channels.

    Next
  3. 3

    Cold flow and checkout

    Run water and stand-in fluids, then check the valves, sensors, and abort.

    Planned
  4. 4

    Hot fire

    Fire the engine, write down the measurements, and inspect the hardware afterward.

    Planned

Work with us

We 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.