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  1. Combustion Characteristics of Stabilized Combustion with Liquid Oxygen Under High Pressure Conditions
  2. The Analytical Study for Operation Condition of Axial-Injection End-Burning Hybrid Rocket
  3. Obtaining C* Efficiency and Establishing Ignition Sequences in Axial-Injection-End-Burning Hybrid Rockets (AIEB-HR) Using Liquid Oxygen
  4. Combustion Characteristics of Stabilized Combustion with Liquid Oxygen at Different Operating Conditions