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Expander cycle
The SKYLON Spaceplane
Rocket Propulsion Fundamentals 2
IAF Space Propulsion Symposium 2019
Fuel and Oxidizer Feed Systems
Basic Analysis of a LOX/Methane Expander Bleed Engine
Experimental Study of the Combustion Efficiency in Multi-Element Gas
Materials for Liquid Propulsion Systems
Development of LE-X Engine,Mitsubishi Heavy Industries
Lox/Lch4 Upper Stage Development Strategies for Future Launchers
Le Rôle Du Cnes Dans L'écosystème Spatial Français
Appendix a Example Engine Cycle Schemes
Technology Challenges for Deep-Throttle Cryogenic Engines for Space Exploration
Expander and Coolant-Bleed Cycles of Methane-Fueled Rocket Engines*
Propulsion System Choices and Their Implications
Liquid Natural Gas Expander Cycle Demonstrator Engine
Component Tests of a LOX/Methane Full-Expander Cycle Rocket Engine: Single-Shaft LOX/Methane Turbopump
Masters Thesis Liquid Rocket Engine.Pdf
(12) United States Patent (10) Patent No.: US 7,900,436 B2 Greene (45) Date of Patent: Mar
Top View
A Performance Analysis of a Rocket Based Combined Cycle (RBCC) Propulsion System for Single-Stage-To-Orbit Vehicle Applications
Component Tests of a LOX/Methane Full-Expander Cycle Rocket Engine: Electrically Actuated Valve
Upper Stage Liquid Propellant Rocket Engine: a Case Analysis
Component Tests of a LOX/Methane Full-Expander Cycle Rocket Engine: Injector and Regeneratively Cooled Combustion Chamber
Parametric Study of Dual-Expander Aerospike Nozzle Upper-Stage Rocket Engine
Design of a Centrifugal Pump for an Expander Cycle Rocket Engine
Expander Demonstrator
Methane Dual Expander Aerospike Nozzle Rocket Engine Michael D
Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
High Performance Lox Hydrogen Upper Stage with Pistonless Pump
(12) United States Patent (10) Patent No.: US 8,572,948 B1 Pinera (45) Date of Patent: Nov
Design of a Dual-Expander Aerospike Nozzle Rocket
High Speed Propulsion Cycles
Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
Space Exploration & Space Colonization Handbook
69674 3 En Bookfrontmatter 1..61
A Single-Stage Reusable Launch Vehicle Concept Abbos Yunusov A