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Flugtriebwerk
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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
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
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
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
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
Plasma Structure of Miniature Ring-Cusp Ion Thruster Discharges
Two-Dimensional Particle-In-Cell Simulation of Magnetic Sails
Ignition Transients in a Scramjet Engine with Air Throttling Part 1: Nonreacting Flow