All Stories

  1. Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance

    Article • Acta Astronautica, May 2024, Elsevier

    Giacomo Gedda, Antonietta Conte

  2. Preliminary study of a resonant igniter for rocket engines

    Article • January 2020, American Institute of Physics

    Prof Dario PASTRONE, Antonietta Conte

  3. Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Antonietta Conte, Prof Dario PASTRONE

  4. Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems

    Article • July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Antonietta Conte, Assistant Professor Jason Rabinovitch

  5. Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors

    Article • July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Antonietta Conte, Assistant Professor Jason Rabinovitch

  6. Design, Modeling and Testing of a O2/CH4 Igniter for a Hybrid Rocket Motor

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Antonietta Conte, Assistant Professor Jason Rabinovitch

  7. Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats

    Article • July 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Antonietta Conte