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
Nitrous Oxide and Oxygen Mixtures (Nytrox) as Oxidizers for Rocket Propulsion Applications
Diffusion- and Kinetics-Limited Combustion of an Explosively Dispersed Aluminum Particle
Predicting Thermoacoustic Instability: A Novel Analytical Approach and Its Experimental Validation
Effects of Orifice Geometry on Gelled Propellants Sprayed from Impinging-Jet Injectors
Flame Transition in Dual-Mode Scramjet Combustor with Oxygen Piloted Ignition
Effects of Plasma Exposure on Boron Nitride Ceramic Insulators for Hall-Effect Thrusters
Oxidation of Ethylene — Air Mixtures at Elevated Pressures, Part 1: Experimental Results
Effect of Oxidizer on the Combustion Performance of Boron-Based Fuel-Rich Propellant
One Method to Increase the Operating Frequency of Pulse Detonation Rocket Engines
FULL-LENGTH PAPERS - Piezoelectric Ignition of Nanocomposite Energetic Materials
Numerical Study of Solid-Rocket Motor Ignition Overpressure Wave Including Infrared Radiation
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
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
Combustion Stability Analysis of Rocket Engines with Resonators Based on Nyquist Plots
Loading Distribution Effects on Separated Flow Transition of Ultra-High-Lift Turbine Blades
Ignition of Fully Dense Nanocomposite Thermite Powders by an Electric Spark
Ignition and Combustion of Boron Particles at One to Ten Standard Atmosphere