The Clementine Attitude Determination and Control System

Paul DeLaHunt, U.S. Naval Research Laboratory
Steve Gates, U.S. Naval Research Laboratory
Marv Levenson, U.S. Naval Research Laboratory
Glenn Creamer, Swales & Associates

2:00 PM

Design and Fabrication of a Low-Cost Composite Spaceframe Spacecraft Structure

John Scherrer, Southwest Research Institute
Gregory Dirks, Southwest Research Institute
Adair Campbell, Texas Composite, Inc.
Robert Sanderson, Texas Composite, Inc.

2:15 PM

Reliable Application of Plastic Encapsulated Microcircuits for Small Satellites

William Ash III, The Johns Hopkins University Applied Physics Laboratory
Eric Hoffman, The Johns Hopkins University Applied Physics Laboratory

2:30 PM

A Low Cost Tailorable Power Source for Microsatellites

Paul Dillard, Boeing Defense & Space Group

2:45 PM

The Clementine Nickel Hydrogen Common Pressure Vessel Battery

Christopher Garner, U.S. Naval Research Laboratory

2:47 PM

Towards Reduced Nickel-Cadmium Battery Cost for Micro Satellites

V. Cavenel, Saft
D. Duquesne, Saft

3:00 PM