PE/N2O Hybrid Rocket Engine (#4)

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Uploaded by on Apr 4, 2011

It consumed 200g N2O and 8g PE in 15 seconds. The N2O injector was a 0.97mm flare jet. Assuming a specific impulse of 1500 Ns/kg, the average thrust would be around 21N. Next time I'll take a 1.85mm flare jet while also increasing the nozzle diameter from 4mm to 5mm.

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