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Materials for Use in Implementing the Written Safety Examination Requirement
Lunar Transient Accelerations White Paper
Occupant Response Analysis of a Full-Scale Crash Test of a Fokker F28 Fellowship Aircraft
Contact with Bennu! Flight Performance Versus Prediction of OSIRIS-REx TAG Sample Collection
Mode Projection Method for Target Mode Identification
Pterodactyl: Non-propulsive Control Systems for Future Planetary Missions
Flutter Prediction for Aircraft Conceptual Design
Nonlinear Analysis of a Two-Parachute System Undergoing Pendulum Motion
Interference Drag Associated with Engine Locations for Multidisciplinary Design Optimization
Summary of Results from a Fokker F-28 Full Scale Crash Test
Human Mars Entry, Descent and Landing Architecture Study: Deployable Decelerators
An Examination of Heater Bar Outgassing
Testing of the Lunar Reconnaissance Orbiter Attitude Control System Re-Design Without a Gyro
Pattern Recognition Control Design
Pattern Recognition Control Design
Sizing and Layout Design of an Aeroelastic Wingbox Through Nested Optimization
Three-Dimensional Modeling of Aircraft High-Lift Components with Vehicle Sketch Pad
HAT Tricks: Understanding Human Autonomy Teaming Through Applications
A Simple Method for High-Lift Propeller Conceptual Design
Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces
High Leverage Technologies for In-Space Assembly of Complex Structures
Overview of the Transport Rotorcraft Airframe Crash Testbed (TRACT) Full Scale Crash Tests
Assessment of Aeroacoustic Simulations of the High-Lift Common Research Model
A Simple Analytic Model for Estimating Mars Ascent Vehicle Mass and Performance
Aeroservoelastic Optimization under Stochastic Gust Constraints
Tennessee Valley Corridor Leadership Council
Dragonfly Entry and Descent Overview
Simulation and Analysis of NASA Lift Plus Cruise eVTOL Crash Test
Parachute Models Used in the Mars Science Laboratory Entry, Descent, and Landing Simulation
Lessons Learned from Large-Scale Aerospace Structural Testing
Lessons Learned from Large-Scale Aerospace Structural Testing
Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration
Development of an Integrated Data Acquisition System for a Small Flight Probe
Orion GN and C Model Based Development: Experience and Lessons Learned
Post-Flight EDL Entry Guidance Performance of the 2011 Mars Science Laboratory Mission
The Effect of Systematic Error in Forced Oscillation Testing
Recent NASA Wake Surfing Flight Research
Sensitivity Analysis for Multidisciplinary Systems (SAMS)
Application of Adjoint Methodology in Various Aspects of Sonic Boom Design
Structures and Mechanisms Design Concepts for Adaptive Deployable Entry Placement Technology
Aerostructural Level Set Topology Optimization for a Common Research Model Wing