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M10 (rocket engine)
First Stage of a Highly Reliable Reusable Launch System
Space in Space
Worldwide Equipment Guide
Paolo Bellomi
Space Projects
Development of the Liquid Oxygen and Methane M10 Rocket Engine for the Vega-E Upper Stage
Installed Performance Evaluation of an Air Turbo-Rocket Expander Engine ∗ V
Optimized Dual Expander Aerospike Rocket Joshua N
Solid Propellants Part One
Multidisciplinary Design Optimization of Reusable Launch Vehicles for Different Propellants and Objectives
Institute of Space Propulsion Lampoldshausen
A Reliable Method for Predicting the Specific Impulse of Chemical Propellants Dany Frem1
High-Elevation Equatorial Catapult-Launched RBCC SSTO Spaceplane for Economic Manned Access to LEO
Methane Dual Expander Aerospike Nozzle Rocket Engine Michael D
Design, Development, and History of the Oxygen/Hydrogen Engine RD
V28 25022021 22H.Xlsx
5. Test Facilities
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