Systems or subsystems that provide a measurable increase in small satellite utility across of range of mission performance requirements with emphasis on: Techniques and methods that could eliminate the “T” in I&T; Standards for component size or form factors to better enable multi-source spacecraft designs; Constellation Standards – Crosslinks, Autonomy, Command and Control Techniques, etc.
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| 2005 | ||
| Monday, August 8th | ||
| 3:15 PM |
Modular Thermal Design Concepts: Thermal Design of a Spacecraft on a Module Level for LEO Missions Mark Barton, AeroAstro, Inc. 3:15 PM |
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|---|---|---|
| 3:30 PM |
Modular Platform Architecture for Small Satellites: Evaluating Applicability and Strategic Issues Quinn Young, Space Dynamics Laboratory 3:30 PM |
|
| 3:45 PM |
A Universal Interface for Modular Spacecraft Lennon Rodgers, MIT 3:45 PM |
|
| 4:00 PM |
Using a Distributed Wiring Harness Steven Wichman, Space Gadgets Corporation 4:00 PM |
|
| 4:15 PM |
Modular Architecture and Product Platform Concepts Applied to Multipurpose Small Spacecraft Jenny Kingston, Cranfield University 4:15 PM |
|
| 4:30 PM |
Optimum Placement of Satellite Components with Genetic Algorithms Ayman Kassem, King Fahd University of Petroleum & Minerals 4:30 PM |
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