Laser Ignition of an Experimental Cryogenic Reaction and Control Thruster: Ignition Energies
Modeling of Ullage Collapse Within Rocket Propellant Tanks at Reduced Gravity
Difficulties in Dual-Mode Operation of Nontoxic Hypergolic Thruster Using Decomposition of
Nitrous Oxide and Oxygen Mixtures (Nytrox) as Oxidizers for Rocket Propulsion Applications
Opening Characteristics of Two-Stage Opening Oxidizer Shut-Off Valve
Temperature and Size Measurements of Cryogenic Spray Droplets with Global Rainbow Refractometry
Parahydrogen–Orthohydrogen Conversion for Enhanced Vapor-Cooled Shielding of Liquid Oxygen Tanks
Numerical Simulation of the Thermal Effect in the Cavitating Venturi Flow
Role of Ignition Delay in Rotating Detonation Engine Performance and Operability
Homogeneous Equilibrium Modeling for Subcritical Flows in Liquid Rocket Engine Cooling Systems
LOx Jet Atomization Under Transverse Acoustic Oscillations
Characteristics of Thermal Cavitation on a Two-Dimensional Hydrofoil
Multidisciplinary Design and Architecture Optimization of a Reusable Lunar Lander
Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement