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Turbopump
Turbopump Design and Analysis Approach for Nuclear Thermal Rockets
Development of Turbopump for LE-9 Engine
6. Chemical-Nuclear Propulsion MAE 342 2016
Materials for Liquid Propulsion Systems
The Modified Fuel Turbopump of 2Nd Stage Engine for H3 Launch Vehicle
Nuclear Propulsionfa Historical Perspective Stanley Gunn*,1 P.O
Preparation of Papers for AIAA Journals
RS-25: the Clark Kent of Engines for the Space Launch System
Space Shuttle Main Engine Orientation
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
Lecture 28: Mechanical Design of Turbomachinery
Experimental Study of the Combustion Efficiency in Multi-Element Gas
Materials for Liquid Propulsion Systems
Development of LE-X Engine,Mitsubishi Heavy Industries
Development of Turbopump for LE-X Engine
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
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
Development Study on Air Turbo-Ramjet for Space Plane
Design and Analysis of a High Speed, High Pressure Peroxide RP-1
CECE: Expanding the Envelope of Deep Throttling Technology in Liquid Oxygen/Liquid Hydrogen Rocket Engines for NASA Exploration Missions
Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
Aerospace Castings
Chapter 2.3.11 Liquid Propulsion: Propellant Feed System Design
Turbopumps for Gas Generator and Staged Combustion Cycle Rocket Engines
Nuclear Thermal Rocket Engine with a Toroidal Aerospike Nozzle
Single-Shaft Turbopumps in Liquid Propellant Rocket Engines
High Speed Propulsion Cycles
Developmental History of Liquid Oxygen Turbopumps for the LE-7 Engine∗
20000068530.Pdf
Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
Intgrated Design Method of a Rocket Engine Turbopump Sub-System for Suppressing Rotor Lateral Vibration
Materials for Advanced Rocket Engine Turbopump Turbine Blades W. T