MARK I

Mark I is Project Wavefront's inaugural design and the world's first long-duration rotating detonation rocket engine designed, built, and operated by students. As a technology demonstrator, it aims to enable future engine and vehicle development.

2 kN

Thrust

30 sec

Burn Time

0.95 MW

Water Cooling

Methagox

Fuel/Oxidizer

255 sec

Specific Impulse (sea-level)

6.5 cm

Chamber Diameter

0.82 kg/s

Propellant Flow Rate

13.5 kHz

Frequency

Overview Render

OVERVIEW

Mark 1 is a cutting-edge rotating detonation rocket engine engineered by Project Wavefront. Designed to reach thermal equilibrium for long-duration hotfires, it pioneers detonation-wave combustion in a compact, reusable, reignitable platform.

KEY SPECS

2 kN
Target Thrust
255 sec
Isp (sea-level)
30 sec
Burn Time
0.82 kg/s
Propellant MFR
0.95 MW
Water Cooling
13.5 kHz
Frequency
Key Specs Render
Front Render

ARCHITECTURE

Featuring an annular combustion chamber with integrated cooling channels, the Mark 1's architecture optimizes detonation propagation, heat transfer, and engine efficiency. The engine is being concurrently developed with an advanced electronic control/data collection suite and a purpose-built test stand.

DETONATION INNOVATION

The RDRE leverages continuous detonation waves to improve thermodynamic efficiency beyond conventional deflagration-based engines. This breakthrough reduces propellant consumption while achieving higher chamber pressures and stable thrust output.

Half Render

MARK I TESTING & ROADMAP

Mark 1 will undergo hot-fire testing on Wavefront's custom-built test stand in Q2 of 2026, aiming to reach thermal equilibrium in the process. Future iterations focus on full-duration burn stability, cryogenic fuel integration, and eventual flight-qualified units for launch vehicle prototypes.

Jun2025
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Jan2026
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Jun2026
Completed
Upcoming