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Materials for Use in Implementing the Written Safety Examination Requirement
Occupant Response Analysis of a Full-Scale Crash Test of a Fokker F28 Fellowship Aircraft
Sensitivity Analysis for Multidisciplinary Systems (SAMS)
Framework for Multidisciplinary Analysis, Design, and Optimization with High-Fidelity Analysis Tools
GN&C Engineering Best Practices for Human-Rated Spacecraft System
Blue Origin De-orbit Descent and Landing Tipping Point: Program Final Report
A Generic Inner-Loop Control Law Structure for Six-Degree-of-Freedom Conceptual Aircraft Design
Experimental Photogrammetric Techniques Used on Five Full-Scale Aircraft Crash Tests
Marshall Space Flight Center Faculty Fellowship Program
Simulation of X-38 Landing Scenarios With Landing Gear Failures
FPI and MPI of Cracks Under Coatings
Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel
Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
Preliminary design of a high speed civil transport: The Opus 0-001
Feasibility study for ergonomic analysis and design of future helicopter cockpit systems
Initial flight qualification and operational maintenance of X-29A flight software
Conceptual design proposal: HUGO global range/mobility transport aircraft
The DELTA MONSTER: An RPV designed to investigate the aerodynamics of a delta wing platform
Autonomous spacecraft maintenance study group
Aircraft energy efficiency laminar flow control glove flight conceptual design study
Cognitive engineering in aerospace applications
Findings of a review of spacecraft fire safety needs
The Guardian: Preliminary design of a close air support aircraft
Space Station Simulation Computer System (SCS) study for NASA/MSFC. Concept document
Exhibit D modular design attitude control system study
Aircraft integrated design and analysis: A classroom experience
CrossTalk: The Journal of Defense Software Engineering. Volume 28, Number 2, March/April 2015
Drop Tower Tests for Munitions
Summary of HCAT Helicopter Dynamic Components Project
Simulation Validation for an Automatic Air Collision Avoidance System in Preparing for Flight Test
Voyager Project Progress Report, Oct. 16 - Nov. 15, 1965
Next Generation Instrumentation Bus Test Plan for Fibre Channel
U.S. Army Research Laboratory (ARL) DESCENT Model Roadmap: Current Scope and Near-Term Extensions
Development of a Tow Capability for the HH-3F Helicopter
Experimental Approach to Determine the Flight Dynamics of NASA's Mars Science Lab Capsule
Navigation, Guidance and Control For the CICADA Expendable Micro Air Vehicle