The Complete Series of NU-LHT Lunar Simulants
Creating a New Airmass RGB for NWS Forecasters with Color Vision Deficiency
Risk and Performance Assessment of Generic Mission Architectures: Showcasing the Artemis Mission
Comparison of Operational S/X and VGOS Sessions for EOP Determination
autoNGC: Autonomous Navigation, Guidance, and Control Software in a Low SWaP Box
Applying Linear Programming to Optimize Fire Station Location
Fluid for Thought: SLS Rocket Aerodynamics featuring Pressure Sensitive Paint
Materials Informatics Enables Rapid Materials Discovery
Current State of NASA Continuously Rotating Detonation Cycle Engine Development
Materials for Extreme Environments: Enabling Advances in Aviation and Space
Visual and Inertial Datasets for an eVTOL Aircraft Approach and Landing Scenario
A New Method For Calibration of High-Capacity Wind Tunnel Force Measurement Instrument
One Giant Leap for Womankind: Studying NASA’s SLS Rocket With Pressure-Sensitive Paint
Orion Heat Shield Manufacturing Producibility Improvements for the EM-1 Flight Test Program
Defining the Required Net Habitable Volume for Long-Duration Exploration Missions
Heliophysics: Prediction of Radiation Doses Received During Airplane Flights
Copper-Water and Hybrid Aluminum-Ammonia Heat Pipes for Spacecraft Thermal Control Applications
Copper-Water and Hybrid Aluminum-Ammonia Heat Pipes for Spacecraft Thermal Control Applications
Participant Training for a Flight Test Evaluation of Interval Management
An Overview of NASA’s Aerosols and Clouds-Convection-Precipitation (A-CCP) Pre-formulation Study
Modeling of a Modern Aircraft Through Calibration Techniques
Implementing CubeSat Avionics Components to Full-Scale Capsule Return Missions
Lean Model-Based Systems Engineering on the NASA High-Density Vertiplex Subproject
Expandable Variable-Autonomy Architecture Viable Maneuver Displays
Logistics Warehouse Facility Utilization Study: Vehicle Processing Support Area (VPSA)
Towards Multiphysics Prediction Capability for the KSC Launch Environment
Predicted Performance of an X-Ray Navigation System for Future Deep Space and Lunar Missions
Aeropropulsive Design Optimization of a Turboelectric Boundary Layer Ingestion Propulsion System
Incorporating Test Data for Small UAS at the Conceptual Design Level