Assessment of Electric-Pump-Fed Nuclear Thermal Propulsion for Near-Term Missions
Current Status of Liquid-Bipropellant Detonation-Based Propulsion Devices
Opening Characteristics of Two-Stage Opening Oxidizer Shut-Off Valve
Progress of CFM Model Development and Validation at NASA Glenn Research Center
Mission Incredible: A Titan Sample Return Using In-Situ Propellants
Testing of TVS Augmented Injectors for Tank-to-Tank Transfer of Cryogens
Thermal Analysis of Cooling Channels on Electromechanical Actuator During Actual Flight
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement
Design Considerations for an Earth–Mars Cycler Spacecraft Using the S1L1 Cycler
Multidisciplinary Design and Architecture Optimization of a Reusable Lunar Lander
Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers
Cryogenic In-Situ Liquefaction for Landers “Brassboard” Liquefaction Testing Series
Space Technology Mission Directorate Game Changing Development Program
Cryogenic Fluid Management Technologies Enabling for the Artemis Program and Beyond
Parametric Design of a Crew Transfer Vehicle for Earth–Mars Cyclers