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Flugtriebwerk
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Editorial Policy Statement on Numerical and Experimental Accuracy
Solid-Fuel Regression Rate Modeling for Hybrid Rockets
Mass and Cost Model for Selecting Thruster Size in Electric Propulsion Systems
Gelled Monomethyl Hydrazine Hypergolic Droplet Investigation
Effect of Trailing Ramp Angles in Strut-Based Injection in Supersonic Flow
Experiments on an Oxidizer-Rich Preburner for Staged Combustion Cycle Rocket Engines
Performance of a Helicon Hall Thruster Operating with Xenon, Argon, and Nitrogen
Numerical Investigation of Dual-Mode Operation in a Rectangular Scramjet Flowpath
Evaluation of Processing and Mechanical Parameters of Dicyclopentadiene-Based Gumstocks
Impacts of Particle Size and Pressure on Reactivity of Boron Oxidation
Thrust Evaluation in Wide Frequency Range Using Active Control and Disturbance Observer
Evaluation of Ethanol-Blended Hydrogen Peroxide Monopropellant on a 10 N Class Thruster
Effects of Limitation of Nozzle Flow Separation on Launcher Performance
Hypersonic Viscous Drag Reduction via Multiporthole Injector Arrays
Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines
Scaling of Miniature Piston-Engine Performance, Part 1: Overall Engine Performance
Effect of Plasma Discharges on Nitric Oxide Emissions in a Premixed Flame
Functionalization and Passivation of Boron Nanoparticles with a Hypergolic Ionic Liquid