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Launch Vehicle and Spacecraft Transmitter Electromagnetic Compatibility
Materials for Use in Implementing the Written Safety Examination Requirement
X-57 Mod II Avionics Power Analysis
Overview of the Acoustic Testing of the European Service Module Structural Test Article (E-STA)
X-57 Cruise Motor and High-Lift Motor Mission Profile Power Analysis
Mode Projection Method for Target Mode Identification
Pterodactyl: Non-propulsive Control Systems for Future Planetary Missions
X-57 Mod IV Avionics Power Analysis
Overview of the Acoustic Testing of the European Service Module Structural Test Article (E-STA)
Overview of the Acoustic Testing of the European Service Module Structural Test Article (E-STA)
Preliminary Design, Testing, and Performance of the LOFTID Navigation System
Summary of Results from a Fokker F-28 Full Scale Crash Test
Contact with Bennu! Flight Performance Versus Prediction of OSIRIS-REx TAG Sample Collection
An Examination of Heater Bar Outgassing
Occupant Response Analysis of a Full-Scale Crash Test of a Fokker F28 Fellowship Aircraft
Lunar Transient Accelerations White Paper
Human Mars Entry, Descent and Landing Architecture Study: Deployable Decelerators
Sizing and Layout Design of an Aeroelastic Wingbox Through Nested Optimization
Nonlinear Analysis of a Two-Parachute System Undergoing Pendulum Motion
Interference Drag Associated with Engine Locations for Multidisciplinary Design Optimization
HAT Tricks: Understanding Human Autonomy Teaming Through Applications
Flutter Prediction for Aircraft Conceptual Design
Pattern Recognition Control Design
Pattern Recognition Control Design
Testing of the Lunar Reconnaissance Orbiter Attitude Control System Re-Design Without a Gyro
A Simple Method for High-Lift Propeller Conceptual Design
Overview of the Transport Rotorcraft Airframe Crash Testbed (TRACT) Full Scale Crash Tests
Assessment of Aeroacoustic Simulations of the High-Lift Common Research Model
High Leverage Technologies for In-Space Assembly of Complex Structures
A Novel UAV Electric Propulsion Testbed for Diagnostics and Prognostics
Three-Dimensional Modeling of Aircraft High-Lift Components with Vehicle Sketch Pad
Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces
Aeroservoelastic Optimization under Stochastic Gust Constraints
Lightweight Innovative Solar Array (LISA): Providing Higher Power to Small Spacecraft
Tennessee Valley Corridor Leadership Council
Far Term Noise Reduction Technology Roadmap for a Large Twin-Aisle Tube-And-Wing Subsonic Transport
A Simple Analytic Model for Estimating Mars Ascent Vehicle Mass and Performance
Post-Flight EDL Entry Guidance Performance of the 2011 Mars Science Laboratory Mission
The Effect of Systematic Error in Forced Oscillation Testing
Thermal Modeling in Support of the Edison Demonstration of Smallsat Networks Project