Research and Development Projects of the CPL

Previous:

1. Design and Fabrication of the Propulsion System That Meets the Requirements of SARA Reentry Platform Using Hybrid Propellants (2013 - 2016)
2. Investigation of Liquid Spray Cooling for Aerospace Applications (2015 - 2017)
3. Experimental Studies of the Thermo-structural Materials Used as the Thermal Insulation for the Hybrid Rocket Engines (2015 - 2018)
4. Design, Development and Testing of the Torch Ignition System for the Hybrid Rocket Motor (2015 - 2018)

Current:

1. Design and Development of a High-Maneuverability Supersonic Missile with Ramjet Engine (2016 - 2019)
2. Thrust Control System for the Hybrid Rocket Motor (2017 - 2020)
3. Development and testing of the digital control valve for the hybrid motor feed system (2017 - 2019)
4. Development of technological process of filament winding for the fabrication of structural elements of the hybrid propulsion rocket engine (2017 - 2019)