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Orbital Debris and the NASA Orbital Debris Program Office
REALM TechPort - The Advanced Exploration Systems, Logistics Reduction Project
Extravehicular Activity and Human Surface Mobility Program (EHP)
SCEPTOR X-57 Maxwell Structural Loads Requirements for Floor and Equipment Support
X-57 Maxwell Structural Loads Requirements Loads Analysis for Cruise Nacelle Structure
Polaris Project: Spaceflight Autonomous Multigenerational Microbial Sequencer (SAMMS)
Hazards of Lunar Surface Exploration: Determining the Immunogenicity/Allergenicity of Lunar Dust
Contribution to the LHP Section of Chapter 14 – Heat Pipes (Spacecraft Thermal Control Handbook)
LESSH Lunar Experiment Support System and Handling Battery Charger Module
Finite Element Model Tuning using Analytical Sensitivity Values
Numerical Investigation of CL,max Prediction on the NASA High-Lift Common Research Model
Testing theories of Gravitation with the Interstellar Probe Radio Experiment
Estimations of Aircraft and Airport Domestic Greenhouse Gas Emissions from 2016-2021
Distributed Sensing Avionics Suite Data from Low Altitude Flights at NASA Ames Research Center
Non-Invasive Ventilation Evaluation in Exploration Missions
Overview of Commercial High-Speed Market Studies and NASA’s Hypersonic Technology Project
Frequency Analysis of UAV Vibration Anomalies Due to Wind (INTERN NOTES)
Importance of Intellectual Curiosity as a Research Engineer
Commercial Low-Earth Orbit Destination (CLD) Capabilities of Interest and Resource Needs
NASA Radiation Hardness Assurance (RHA) Standard: Status for 2023 NEPP ETW
Multifunctional End Effector for Regolith Construction, Acquisition, and Transfer (MEERCAT) Flyer
Human Landing System (HLS) Program Non-Design Driver Lunar Environments
Payload Topology Forum: IVA Payload Placement Process and Timeline
Kamodo: Simplifying Model Data Access and Utilization
Fault Detection and Diagnosis in Spacecraft Electrical Power Systems
2023 NASA Engineering & Safety Center (NESC) Technical Update
Equivalent Area Targets for Inverse Design Optimization With Changing Low-Boom Cruise Conditions
Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
Propulsion-Airframe Integration for Conceptual Redesign of a Low-Boom Supersonic Transport