Use of the Landing Point Designator to Land the Lunar Module to a Given Target - Project APOLLO
Space Shuttle Ascent Flight Design Process: Evolution and Lessons Learned
Benefits of Low-Power Stationary Plasma Thruster Propulsion for Small Satellites
Satellite Contamination and Materials Outgassing Knowledge base
Bordautonomous Terrain Aided Flight Navigation in Height Sections Close to Terrain Surface
Assessment of Data Handling Configurations for Onboard Operating System Definition (Phase 1)
The Small Scientific Satellite ( S Sup 3) Program and Its First Payload
Onboard diagnosis of the drive circuit of an electronically controlled injector
Current Trends toward the Improvement of Scientific Instruments for Weather Satellite Application