Research and Development Projects of the CPL
Research and Development Projects of the CPL
Previous:
Previous:
- Design and Fabrication of the Propulsion System That Meets the Requirements of SARA Reentry Platform Using Hybrid Propellants (2013 - 2016)
- Investigation of Liquid Spray Cooling for Aerospace Applications (2015 - 2017)
- Experimental Studies of the Thermo-structural Materials Used as the Thermal Insulation for the Hybrid Rocket Engines (2015 - 2018)
- Design, Development and Testing of the Torch Ignition System for the Hybrid Rocket Motor (2015 - 2018)
Current:
Current:
- Design and Development of a High-Maneuverability Supersonic Missile with Ramjet Engine (2016 - 2019)
- 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 - 2019)
- Development of technological process of filament winding for the fabrication of structural elements of the hybrid propulsion rocket engine (2017 - 2019)