rootbrowseIAC-04Ssession 11. Propulsion Systems 1Papers1. Development Status of the VINCI Engine of the ARIANE 5 upper Stage2. Development of the Liquid Oxygen/Kerosene Staged Combusion Rocket Engine3. LOX/CH4 Expander Upper Stage Engine4. Advanced Expander Engine5. Test Results for a Non-Toxic Dual Thrust Reaction Control Engine6. Re-using Hardware for Cost, Risk and Schedule Reduction - The Example of the Ariane 5 Cryogenic Upper Stage ESC-A7. Use of Available Satellite Propulsion System Hardware for Launcher Improvement8. Advanced Low Cost Propulsion Concepts for Small Satellites beyond LEO9. The Use of the Aerojet MR-103H Thruster on the New Horizons Mission to Pluton10. Pneumopump-fed Liquid Rocket Engine. Test Results