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Staged combustion cycle
IAF Space Propulsion Symposium 2019
Basic Analysis of a LOX/Methane Expander Bleed Engine
Space Shuttle Main Engine Orientation
Experimental Study of the Combustion Efficiency in Multi-Element Gas
Materials for Liquid Propulsion Systems
Lox/Lch4 Upper Stage Development Strategies for Future Launchers
IAF Committee Briefs
Up of Main Liquid Propellant Engine Under Hot Test Conditions
RWTH Aachen University Institute of Jet Propulsion and Turbomachinery
Implications of Cycle Variants, Propellant Combinations and Operating Regimes on Fatigue Life Expectancies of Liquid Rocket Engines
Incorporation of RD-180 Failure Response 2011
Propulsion System Choices and Their Implications
Cryogenic Rocket Engine
Deutsche Forschungsanstalt Fiir Luft- Und Raumfahrt DLR Lampoldshausen Research Centre Space Propulsion Division D-74239 Hardthausen A.K., Germany 1
Masters Thesis Liquid Rocket Engine.Pdf
RD-180 Engine: an Established Record of Performance and Reliability on Atlas Launch Vehicles Brooke Mosley United Launch Alliance Littleton Colorado
Staged Combustion Cycle Rocket Engine Subsystem Definition for Future Advanced Passenger Transport Martin Sippel, Tobias Schwanekamp
[email protected]
Tel
Upper Stage Liquid Propellant Rocket Engine: a Case Analysis
Top View
Masters Thesis: Liquid Rocket Analysis (Lira)
Lecture 12 Liquid Rocket Propulsion
IAF2010 Paper Spaceliner
The RD-180 Replacement and the Future of the U.S. Rocket Motor Industrial Base
Bibliography No. 39-3
Advanced Rocket Engines
A Liquid Propulsion Panorama
Turbopumps for Gas Generator and Staged Combustion Cycle Rocket Engines
Advanced High Pressure Engine Study for Mixed-Mode Vehicle Applications
Considerations in Designing the Air-Breathing Engines for an STS
Design of a Dual-Expander Aerospike Nozzle Rocket
High Speed Propulsion Cycles
Hydrocarbon Rocket Engines Relevant US Industry Experience
Space Exploration & Space Colonization Handbook