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S400 (rocket engine)
Los Motores Aeroespaciales, A-Z
Effects of Lip Thickness and Recess Length on Spray Characteristics in Gas Centered Double Swirl Injector for 400N Methane Rocket Engine
Motor A-Z 2014V9.1.Indd
ARMADA Finalr Eview
7Th International Symposium on Launcher Technologies
Global Counterspace Capabilities —
Architecting a Family of Space Tugs Based on Orbital Transfer Mission Scenarios
Development Liquid Rocket Engine of Small Thrust with Combustion Chamber from Carbon - Ceramic Composite Material
Dual Lunar Ice Analyzers Supporting Next-Gen Astronautics
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