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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
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
Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets
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
Plasma-Induced Erosion on Ceramic Wall Structures in Hall-Effect Thrusters
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
Dual-Mode Scramjet Flameholding Operability Measurements
Effect of Density Gradient on Flame — Acoustic Interaction
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
Ethical Standards for Publication of Aeronautics and Astronautics Research
Numerical Study of Solid-Rocket Motor Ignition Overpressure Wave Including Infrared Radiation