About Juno
Project Juno is ERPL’s first endeavor into liquid bi-propellant rocket engines in over a decade. This engine was built to be rapidly tested for short duration test fires. Juno was designed to use liquid oxygen and ethanol for propellants but can easily swapped for other fuels.
Juno is currently awaiting testing following a redesign of the igniter assembly.
Engine Specs
- Thrust – 350 lbf
- Chamber Pressure – 450 psia
- Mass Flow Rate – 0.66 kg/s
- Mixture Ratio – 1.3
- Injection Type – Unlike Impinging
Project Contact
Samir Ahmed – [email protected]
Devin Sirota – [email protected]