Project Details
Goal of the project
This project investigates the feasibility of a new type of hybrid rocket propulsion, combining a solid oxygen generator with an inert fuel grain, achieving the safety and performance of conventional hybrid rockets with the simplicity and launch-readiness of solid rocket motors. The proposed technology can find applications both in the Responsive Space domain and for Insensitive Munitions.
Funding acknowledgement
The project DAP/26-10 - HySCORE is funded under the DFR call.
| Acronym | HySCORE |
|---|---|
| Status | Not started |
| Effective start/end date | 1/09/26 → 31/08/30 |
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