Experimental Aero-Physics Branch Fluid Mechanics Laboratory
NASA Perspectives on Deployable Gossamer Space Structures
The Quest for Engineering Innovation at NASA's Marshall Space Flight Center
Utilizing Tissue Engineering and 3D Models to Address Space Exploration Risks
NASA Capacity Building Program Intern Team Findings Final Report
Development of Technical Requirements for On-Board Cryogenic Fuel Systems of Belaz Dump Trucks
NASA, Space, & Spaceship Heatshield Engineering
Human Physiology, Performance, Protection, and Operations (H-3PO) Lab
Distributed Spacecraft Autonomy (DSA)
UAV Delivery Monitoring System
Practical Use of the Braking Attributes Measurements Results
Highly passable propulsive device for UGVs on rugged terrain
History at the NASA Johnson Space Center
Vehicle fuel consumption prediction based on the data record obtained from an engine control unit
Braking Control for Improving Ride Comfort
Observations over 3 Decades: What it takes to Mature and Mission Infuse TPS Technologies at NASA?
Development of Advanced Conformal and Soft Pica for Future Nasa Missions and Commercial Space
Search & Rescue Intelligent Terminal (SAINT) Revolutionizing Search and Rescue Operations
The impact of a vehicle braking system state on safe driving – part one
Modeling Entry Systems to Explore Our Solar System
The Synthesis of Electric Drives Characteristics of the UAV of “Convertiplane–Tricopter” Type
A Relationship between Tyre Pressure and Rolling Resistance Force under Different Vehicle Speed
Golf cart prototype development and navigation simulation using ROS and Gazebo
REALM TechPort - The Advanced Exploration Systems, Logistics Reduction Project
Skid resistance demands of asphalt pavement during the braking process of autonomous vehicles
Experimental research in automobile non-pneumatic tire force heterogeneity
Optimal civil aircraft missions exploiting free routing possibilities
Examination of Doppler Fiber Optic Sensing for Structural Velocity Estimations
Aircraft Path Planning under Adverse Weather Conditions
NASA’s Entry, Descent and Landing (EDL) Background and Demonstration Needs
Aerodynamic Modelling and Analysis of a Novel Mechanism for Chord and Camber Morphing Wing