All Stories

  1. Evaluation of Paraffin–Polyethylene Blends as Novel Solid Fuel for Hybrid Rockets

    Article • Journal of Propulsion and Power, November 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hee Jang Moon, Dr. SOOJONG KIM

  2. Thermal characterizations of the paraffin wax/low density polyethylene blends as a solid fuel

    Article • Thermochimica Acta, August 2015, Elsevier

    Dr. SOOJONG KIM

  3. Mass Transfer Number Sensitivity on the Fuel Burning Rate in Hybrid Rockets

    Article • Journal of Propulsion and Power, July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hee Jang Moon, Jungpyo Lee, Dr. SOOJONG KIM

  4. Inlet Geometry and Equivalence Ratio Effects on Combustion in a Ducted Rocket

    Article • Journal of Propulsion and Power, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Benveniste Natan, Dr. SOOJONG KIM

  5. Regression Characteristics of the Cylindrical Multiport Grain in Hybrid Rockets

    Article • Journal of Propulsion and Power, May 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  6. Effect of a Midst Mixing Chamber on Fuel Regression of a Laboratory Scale Hybrid Rocket Motor

    Article • July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  7. Investigation on the Effect of Liquefying Diaphragm in Hybrid Rocket Motors using Paraffin-Based Fuel

    Article • July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  8. Empirical Estimation of Entrainment Regression Rate in Liquefying Solid Fuel for Hybrid Rocket Motor

    Article • July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  9. Experimental Investigations of Tapered Fuel Regression Rate of Hybrid Rocket Motor

    Article • July 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  10. Effect of Paraffin-LDPE Blended Fuel on the Hybrid Rocket Motor

    Article • July 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  11. A Study on Burning Rate with Mass Transfer Number (B Number) of Solid Fuel in Single Port Hybrid Rocket

    Article • July 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM

  12. Combustion Characteristics of the Cylindrical Multi-Port Grain for Hybrid Rocket Motor

    Article • August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. SOOJONG KIM