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Vulcain (rocket engine)

  • Numerical Investigation of a 7-Element GOX/GCH4 Subscale Combustion Chamber

    Numerical Investigation of a 7-Element GOX/GCH4 Subscale Combustion Chamber

  • Qualification Over Ariane's Lifetime

    Qualification Over Ariane's Lifetime

  • Materials for Liquid Propulsion Systems

    Materials for Liquid Propulsion Systems

  • Los Motores Aeroespaciales, A-Z

    Los Motores Aeroespaciales, A-Z

  • Aerospace Science and Technology 86 (2019) 444–454

    Aerospace Science and Technology 86 (2019) 444–454

  • DEVELOPMENT STATUS of the VULCAIN THRUST Chambert

    DEVELOPMENT STATUS of the VULCAIN THRUST Chambert

  • A Methodology for Preliminary Sizing of a Thermal and Energy Management System for a Hypersonic Vehicle

    A Methodology for Preliminary Sizing of a Thermal and Energy Management System for a Hypersonic Vehicle

  • A Survey of Automatic Control Methods for Liquid-Propellant Rocket Engines

    A Survey of Automatic Control Methods for Liquid-Propellant Rocket Engines

  • Materials for Liquid Propulsion Systems

    Materials for Liquid Propulsion Systems

  • IAF Committee Briefs

    IAF Committee Briefs

  • Effect of Bipropellant Combustion Products on the Rocket Nozzle Design

    Effect of Bipropellant Combustion Products on the Rocket Nozzle Design

  • Disrupting Launch Systems

    Disrupting Launch Systems

  • Investigations of Future Expendable Launcher Options

    Investigations of Future Expendable Launcher Options

  • Transient Three-Dimensional Side-Load Analysis of a Film-Cooled Nozzle

    Transient Three-Dimensional Side-Load Analysis of a Film-Cooled Nozzle

  • Development of the Liquid Oxygen and Methane M10 Rocket Engine for the Vega-E Upper Stage

    Development of the Liquid Oxygen and Methane M10 Rocket Engine for the Vega-E Upper Stage

  • Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads

    Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads

  • Appendix a Example Engine Cycle Schemes

    Appendix a Example Engine Cycle Schemes

  • The Ariane 6 Engines Are Now Ready

    The Ariane 6 Engines Are Now Ready

Top View
  • Rocket Engines: Turbomachinery
  • The European Research and Test Site for Chemical Space Propulsion Systems
  • Motor A-Z 2014V9.1.Indd
  • VULCAIN®2.1, the European Reference for Ariane 6 Lower Stage Cryogenic Propulsive System P
  • CNES FUTURE LAUNCHER ROADMAP LA SAPIENZA – May 7Th, 2019 CNES FUTURE LAUNCHER ROADMAP - LA SAPIENZA – MAY 7TH, 2019 Content
  • Space Launch Report Ariane 5 Data Sheet
  • Cryogenic Propulsion Stage
  • Masters Thesis Liquid Rocket Engine.Pdf
  • Maneuvers to Reduce Ariane 5 Upper Stage Lifetime Duration in Orbit
  • Chamber Valve Characteristic
  • Modeling and Simulation of Launch Vehicles Using Object-Oriented Programming
  • PROMETHEUS: Precursor of New Low-Cost Rocket Engine Family
  • VINCI®, the European Reference for Ariane 6 Upper Stage Cryogenic Propulsive System
  • Launcher Evolution Space Rendezvous KTH 2016 Li Forsberg | 13 October 2016 Rev.22 This Document Contains No Technical Data
  • Spacecraft Propulsion.Pdf
  • Toward the Chill-Down Modeling of Cryogenic Upper-Stage Engines Under Microgravity Conditions Using the Thermal-Hydraulic Code COMETE G.-M
  • Consequences of Modeling Demands on Numerical Rocket Thrust Chamber Flow Simulation Tools
  • Advanced Rocket Engines


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