Uploaded August 2016 | Updated September 2026, 2 weeks ago

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Slightly improved version of our 10000 N Hybrid Rocket Engine "HyRES". Compared to last year, we increased the combustion effficiency even further and also the combustion is more stable.

Test 17 with 15 seconds burn time at full thrust. Propellants are Nitrous oxide and paraffin fuel.

Built with funding from the German STERN Program from the DLR. Test site M11.5 provided from DLR Lampoldshausen. To be launched on the sounding rocket HEROS 2 from Esrange, Sweden.

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