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Turbopump

  • Turbopump Design and Analysis Approach for Nuclear Thermal Rockets

    Turbopump Design and Analysis Approach for Nuclear Thermal Rockets

  • Development of Turbopump for LE-9 Engine

    Development of Turbopump for LE-9 Engine

  • 6. Chemical-Nuclear Propulsion MAE 342 2016

    6. Chemical-Nuclear Propulsion MAE 342 2016

  • Materials for Liquid Propulsion Systems

    Materials for Liquid Propulsion Systems

  • The Modified Fuel Turbopump of 2Nd Stage Engine for H3 Launch Vehicle

    The Modified Fuel Turbopump of 2Nd Stage Engine for H3 Launch Vehicle

  • Nuclear Propulsionfa Historical Perspective Stanley Gunn*,1 P.O

    Nuclear Propulsionfa Historical Perspective Stanley Gunn*,1 P.O

  • Preparation of Papers for AIAA Journals

    Preparation of Papers for AIAA Journals

  • RS-25: the Clark Kent of Engines for the Space Launch System

    RS-25: the Clark Kent of Engines for the Space Launch System

  • Space Shuttle Main Engine Orientation

    Space Shuttle Main Engine Orientation

  • Design Procedure of a Turbopump Test Bench Julian Pauw, Lucrezia Veggi, Bernd Wagner, Joydip Mondal, Maximilian Klotz, Oskar Haidn

    Design Procedure of a Turbopump Test Bench Julian Pauw, Lucrezia Veggi, Bernd Wagner, Joydip Mondal, Maximilian Klotz, Oskar Haidn

  • 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

  • Lecture 28: Mechanical Design of Turbomachinery

    Lecture 28: Mechanical Design of Turbomachinery

  • Experimental Study of the Combustion Efficiency in Multi-Element Gas

    Experimental Study of the Combustion Efficiency in Multi-Element Gas

  • Materials for Liquid Propulsion Systems

    Materials for Liquid Propulsion Systems

  • Development of LE-X Engine,Mitsubishi Heavy Industries

    Development of LE-X Engine,Mitsubishi Heavy Industries

  • Development of Turbopump for LE-X Engine

    Development of Turbopump for LE-X Engine

  • Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages

    Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages

  • Nuclear Thermal Propulsion Systems (Last Updated in January 2021) Eric PROUST Eric Proust

    Nuclear Thermal Propulsion Systems (Last Updated in January 2021) Eric PROUST Eric Proust

Top View
  • Optimization and Application of Cryogenic/Thermal Insulation Design for a Liquid-Propellant Rocket Engine
  • Technology Challenges for Deep-Throttle Cryogenic Engines for Space Exploration
  • Rocket Engines: Turbomachinery
  • RS-25 Incredible Facts
  • The Survey of Space Shuttle
  • FS&T Template
  • Development of Highly Competitive Liquid Rocket Engines in Time of Space Gold Rush
  • Advancing Europe's Hybrid Rocket Engine Technology with Paraffin
  • HYBRID PROPELLANT ROCKETS Terry A
  • RL10A-3-3A Rocket Engine Modeling Project
  • Advanced Ramjet Concepts Program
  • Upper Stage Liquid Propellant Rocket Engine: a Case Analysis
  • The Concept Design of a Split Flow Liquid Hydrogen Turbopump
  • ITEM 3 Propulsion Components and Equipment Propulsion Components And
  • Additive Manufacture of Propulsion Systems in Low Earth Orbit
  • An RL10A-3-3A Rocket Engine Model Using the Rocket Engine Transient Simulator (ROCETS) Software
  • Transient Simulation of the Rl-10A-3-3A Rocket Engine
  • Next-Generation RS-25 Engines for the NASA Space Launch System


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