Race2Space — 2024–2025

PHYRE (Peryton Hybrid Rocket Engine) cold-flow testing with liquid N₂O up to 50 bar. Igniter-port leak informed design changes ahead of combustion-chamber integration and the planned hot-fire of PHYRE V1, with knowledge transfer to the next cohort.

• Cold-flow test to 50 bar N₂O
• Igniter-port leak identified for redesign
• Hot-fire of PHYRE V1 in preparation; team handover underway