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Fuel Optimal Guidance Law for Space Vehicles and Its Application to Soft Landing on the Moon
Aerodynamic Characteristics of a Plate at an Angle of Attack in a Viscous Hypersonic Flow
A Vehicle Borne Acceleration Integrator for Computing Velocity Data
Planning for Space Station Freedom Laboratory Payload Integration
Transonic Aeroelastic Calculations in Both the Time and Frequency Domains
Advancing Automation and Robotics Technology for the Space Station Freedom and for the US Economy
GIS and Time-Series Integration in the Kennedy Space Center Environmental Information System
Meteoroids and Orbital Debris: Effects on Spacecraft
Java-based Graphical User Interface for MAVERIC-II