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RAKETENANTRIEB
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keywords:(RAKETENANTRIEB)
Assessment of a liquid rocket engine concept based on innovative technologies
Integrated Fluid — Structure Simulation for Full Burning of a Solid-Propellant Rocket Interior
Influence of Fe2O3 Size on Burning Characteristics of Ammonium Nitrate/ Fe2O3 Propellants
Suppressing a High-Frequency Instability with Varying Bands of White Noise
Surface Instability on Cryogenic Swirl Flow at Sub- to Supercritical Conditions
Radiation and Roughness Effects on Nozzle Thermochemical Erosion in Solid Rocket Motors
SURVEY PAPERS - Review of Worldwide Activities in Liquid-Fed Pulsed Plasma Thruster
Platinum/Barium Hexaaluminate Catalyst to Small-Scale Hydroxylamine Nitrate Thrusters Application
Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter
Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers
Prediction of Combustion Noise for an Aeroengine Combustor
Demonstration of Compact Air Separation Technology for In-Flight Oxygen Collection Space Launchers
Experimental Techniques to Study Linear Burning Rates of Heterogeneous Liquid Monopropellants
Thrust Measurements of the Gaia Mission Flight-Model Cold Gas Thrusters
Laser Ignition of an Experimental Cryogenic Reaction and Control Thruster: Pre-Ignition Conditions
Distortion Management in a Boundary Layer Ingestion Inlet Diffuser Using Hybrid Flow Control
Aeroacoustics of Three-Stream High-Speed Jets from Coaxial and Asymmetric Nozzles