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
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