Environmental Control Systems for Exploration Missions One and Two
Cryogenic Propellant Storage and Transfer Technology Demonstration Mission
After Math - Foamology and Flight Rationale
Improved assessment of aviation hazards to ground facilities using a geographical information system
Simulation Assisted Risk Assessment Applied to Launch Vehicle Conceptual Design
Oceanic Surveillance and Navigation Analysis, FY 71
Simulation of X-38 Landing Scenarios With Landing Gear Failures
Forecasting Aircraft Mishaps Using Monthly Maintenance Reports
Dynamic Modeling of Ascent Abort Scenarios for Crewed Launches
Collision Risk Related to the Usage of Parallel Runways for Landing
Accident Prediction Model Development: Signalized Intersections
Modelling the Low Earth Space Debris Environment
Driving Speeds and Pedestrian Safety: A Mathematical Model