Previous:
- Design and Fabrication of the Propulsion System That Meets the Requirements of the SARA Reentry Platform Using Hybrid Propellants (2013 - 2016)
- Experimental Studies of the Thermo-structural Materials Used as the Thermal Insulation for the Hybrid Rocket Engines (2015 - 2018)
- Investigation of Liquid Spray Cooling for Aerospace Applications (2015 - 2017)
- Design, Development, and Testing of the Torch Ignition System for the Hybrid Rocket Motor (2015 - 2018)
- Design and Development of a High-Maneuverability Supersonic Missile with a Ramjet Engine (2016 - 2019)
- Combustion Instability in Hybrid Rocket Propulsion Systems (2013 - 2018)
- Thrust Control System for the Hybrid Rocket Motor (2017 - 2020)
- Development and testing of the digital control valve for the hybrid motor feed system (2017 - 2020)
- Development of the technological process of filament winding for the fabrication of structural elements of the hybrid propulsion rocket engine (2017 - 2020)
- Academic rocket construction with 3 km apogee (2020 - 2022).
Current:
- Development of a vertical bench for hybrid rocket engines (2021 - 2023)
- Development and testing of thrust vectoring system for rocket engines (2021 - 2024)
- Scientific and technical support in rocket development for DeltaV Space Engineering Ltda (2023 - 2025)
- Development and testing of a hybrid propellant rocket engine fabricated by additive manufacturing (2023 - 2026)
- Research on computational and experimental validation methodologies for liquid rocket propulsion (2024 - 2026)