Hybrid rocket engine test (with TVC gimbal)
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- Опубликовано: 11 сен 2024
- Test of the hybrid rocket engine SARA v2, designed for use in the TVC (thrust vector control) project funded by FAPDF and CNPq. The propellants are N2O and paraffin, with a thrust of 1 kN. The engine was tested for 5 seconds to confirm system integrity.
The main achievements are as follows:
- The lightweight engine structure, interfaces, and gimbal sustained dynamic and thermal loads.
- The integrity of heat protection was maintained.
- The nozzle temperature remained within safety limits.
- Design thrust, mass flow rate, and chamber pressure were achieved through real-time valve control.