ENGINES

osprey Engine

osprey mk i

Nitrous Oxide & Isopropyl Alcohol

90% C* Efficiency

6000N Thrust

2400 °C

our first engine…

Osprey’s liquid bi-propellant engine is DUSF’s first liquid engine and the first time we have competed at the Race2Space national propulsion competition.

The engine utilises cooling channels printed into the thrust chamber itself to prevent melting of the chamber walls.

The propellants are delivered through a triplet impinging injector, which reached combustion efficiencies of over 90%, while the total efficiency reached 194s.

The engine and injector were additively manufactured from AlSi10Mg in partnership with Aconity3D.

Thankful to our dedicated team members, Sponsors and many others!