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