NASA’s Developments in Cryogenic Fluid Management Technology
Equivalent Dynamic of Liquid Sloshing Coupled with Mass Transfer During On-Orbit Refueling
Hydrogen Densification for Nuclear Thermal Propulsion Missions
Hydrogen peroxide for propulsive power -- Production and use by Germans during world war II
Inverted Outflow Ground Testing of Cryogenic Propellant Liquid Acquisition Devices
Combustion instabilities in liquid rocket engines : testing and development practices in Russia
Parametric Analysis of Cooling Properties of Candidate Expander-Cycle Fuels
Modeling Fuel Film Cooling on a Flat Plate
High Energy Density Additives for Hybrid Fuel Rockets to Improve Performance and Enhance Safety
Investigating the Explosive Hazard of Liquid Oxygen-Liquefied Natural Gas Rocket Propellant
Characterization of the Hypergolic Ignition Delay of Ammonia Borane
Inverted Outflow Ground Testing of Cryogenic Propellant Liquid Acquisition Devices
Stabilization of Tethered Tug–Debris System with Residual Liquid Fuel
Difficulties in Dual-Mode Operation of Nontoxic Hypergolic Thruster Using Decomposition of
Numerical Study of Spray Combustion Effects on Detonation Propagation
Attitude Dynamics of Spacecraft with Time-Varying Inertia During On-Orbit Refueling
Toward New Horizons. Volume 7. Aircraft Fuels and Propellants