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
Combustion of Aluminum Suspensions in Hydrocarbon Flame Products
LOx Jet Atomization Under Transverse Acoustic Oscillations
Performance Analysis of Composite Propellant Based on HTPB-DNCB
Effect of External Cathode Azimuthal Position on Hall-Effect Thruster Plume and Diagnostics
TECHNICAL NOTES - Compressor Vane Clocking Effects on Embedded Rotor Performance
Influence of Unsteadiness on the Analysis of Pressure Gain Combustion Devices
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
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
Closed-Loop Precision Throttling of a Hybrid Rocket Motor
CoMn-Based Oxides as Bulk Catalyst for Rocket-Grade Hydrogen Peroxide Decomposition
Dual-Pump Coherent Anti-Stokes Raman Spectroscopy Measurements in a Dual-Mode Scramjet
Influence of Ammonia Borane on the Stability of a Liquid Rocket Combustor
Performance Characteristics of Micro-cathode Arc Thruster
Mean-Flow and Acoustic Characteristics of Cold Jets from a Rectangular Hypersonic Nozzle
Full Particle-In-Cell Simulation Methodology for Axisymmetric Hall Effect Thrusters
Sensitivity of Multistage Compressor Performanee to Inlet Boundary Conditions
Tomographic Imaging of Flames: Assessment of Reconstruction Error Based on Simulated Results
Multiphase Investigation of Water Hammer Phenomenon Using the Full Cavitation Model
Mechanistic Assessment of Swirl Coaxial Injection by Quantitative X-Ray Radiography
Power Deposition into the Discharge Channel of a Hall Effect Thruster
Experimental and Numerical Multiphase-Front Fluid Hammer
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