DIY rocket engine slow motion - ONE|AEROSPACE static fire

[@notmadrocketscientist1902]

Very nice! No combustion instabilities. Maybe nozzle exit is a bit too small (like in my rocket engines).

[@oneaerospace8022]

Thank you! We enjoy your videos very much, great work! That is true, for this test we only used a converging nozzle to measure the chamber thrust and determine the best diverging nozzle geometry. More test videos with the finished nozzle to follow soon!