Mechanistic Assessment of Swirl Coaxial Injection by Quantitative X-Ray Radiography
Reactive, Mechanically Alloyed Al . Mg Powders with Customized Particle Sizes and Compositions
Increasing Reliability of a Two-Stroke Internal Combustion Engine for Dynamically Changing Altitudes
Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
TECHNICAL NOTES - Direct-Drive System Demonstration for a Low-Power Hall Thruster
Wall Temperature Effects on Heat Transfer Coefficient for High-Pressure Turbines
Damping Coefficient Prediction of Solid Rocket Motor Nozzle Using Computational Fluid Dynamics
Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description
Prediction and Analysis of Combustion Instabilities in a Model Rocket Engine
Laser Ignition of an Experimental Cryogenic Reaction and Control Thruster: Ignition Energies
TECHNICAL NOTES - Experimental Study on Ignition Process of a Magnesium-Based Water Ramjet Engine
Novel Manufacturing Method for Hydrogen Peroxide Catalysts: A Performance Verification
Enhancing Composite Solid Propellant Burning Rates with Potassium Doped Ammonium Perchlorate-Part I
Parametric Analysis of Cooling Properties of Candidate Expander-Cycle Fuels
Burning Rate Optimization Under Uncertainty Using Response Surfaces and Monte Carlo Simulation
FULL-LENGTH PAPERS - Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics
Ignition Transients in a Scramjet Engine with Air Throttling Part 1: Nonreacting Flow
Nitrous Oxide and Oxygen Mixtures (Nytrox) as Oxidizers for Rocket Propulsion Applications
Diffusion- and Kinetics-Limited Combustion of an Explosively Dispersed Aluminum Particle
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
Predicting Thermoacoustic Instability: A Novel Analytical Approach and Its Experimental Validation
Effects of Orifice Geometry on Gelled Propellants Sprayed from Impinging-Jet Injectors