Satellite Systems Design/Simulation Environment: A Systems Approach to Pre-Phase A DesignA toolset for the rapid development of small satellite systems has been created. The objective of this tool is to support the definition of spacecraft mission concepts to satisfy a given set of mission and instrument requirements. The objective of this report is to provide an introduction to understanding and using the SMALLSAT Model. SMALLSAT is a computer-aided Phase A design and technology evaluation tool for small satellites. SMALLSAT enables satellite designers, mission planners, and technology program managers to observe the likely consequences of their decisions in terms of satellite configuration, non-recurring and recurring cost, and mission life cycle costs and availability statistics. It was developed by Princeton Synergetic, Inc. and User Systems, Inc. as a revision of the previous TECHSAT Phase A design tool, which modeled medium-sized Earth observation satellites. Both TECHSAT and SMALLSAT were developed for NASA.
Document ID
20040105652
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Ferebee, Melvin J., Jr. (NASA Langley Research Center Hampton, VA, United States)
Troutman, Patrick A. (NASA Langley Research Center Hampton, VA, United States)
Monell, Donald W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1997
Subject Category
Communications And Radar
Report/Patent Number
AIAA Paper 97-0231Report Number: AIAA Paper 97-0231
Meeting Information
Meeting: 34th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 6, 1997
End Date: January 9, 1997
Sponsors: American Inst. of Aeronautics and Astronautics