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  • IAC-23
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  • session 2
  • 2. Liquid Propulsion (2)

    Papers

    1. Qualification of a Propulsion System for active Deorbit

    2. Performance Evaluation of Hypergolic Ionic Liquid-based Fuel (ILethCu01) with 95% Hydrogen Peroxide Oxidizer in 50 N Thruster.

    3. Experimental investigation of fuel transverse injection during throttling in a bipropellant thruster.

    4. Employing carbon-split pore tubes as adsorbents to control the leakage of methane in transport valves

    5. SOFT FLOW METER FOR MISSION-ONBOARD TO MEASRUE FLOW PARAMETER FOR LIQUID ROCKET ENGINES

    6. DESIGN AND ANALYSIS OF A NOVEL SWIRL-PINTLE COMBINED FUEL INJECTOR FOR IMPROVED PERFORMANCE OF LIQUID ROCKET ENGINES

    7. Feasibility of UV induced decomposition of High Test Peroxide in spacecraft propulsion.

    8. Performance testing of 1N Hydrogen Peroxide thruster at FOTEC propulsion test facilities

    10. Convective and Radiative Wall Heat Transfer Evaluation in Film-Cooled Liquid Rocket Thrust Chambers