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Modular, Reconfigurable, and Rapid Response Space Systems: The Remote Sensing Advanced Technology MicrosatelliteModular, Reconfigurable, and Rapid-response (MR(sup 2)) space systems represent a paradigm shift in the way space assets of all sizes are designed, manufactured, integrated, tested, and flown. This paper will describe the MR(sup 2) paradigm in detail, and will include guidelines for its implementation. The Remote Sensing Advanced Technology microsatellite (RSAT) is a proposed flight system test-bed used for developing and implementing principles and best practices for MR(sup 2) spacecraft, and their supporting infrastructure. The initial goal of this test-bed application is to produce a lightweight (approx. 100 kg), production-minded, cost-effective, and scalable remote sensing micro-satellite capable of high performance and broad applicability. Such applications range from future distributed space systems, to sensor-webs, and rapid-response satellite systems. Architectures will be explored that strike a balance between modularity and integration while preserving the MR(sup 2) paradigm. Modularity versus integration has always been a point of contention when approaching a design: whereas one-of-a-kind missions may require close integration resulting in performance optimization, multiple and flexible application spacecraft benefit &om modularity, resulting in maximum flexibility. The process of building spacecraft rapidly (< 7 days), requires a concerted and methodical look at system integration and test processes and pitfalls. Although the concept of modularity is not new and was first developed in the 1970s by NASA's Goddard Space Flight Center (Multi-Mission Modular Spacecraft), it was never modernized and was eventually abandoned. Such concepts as the Rapid Spacecraft Development Office (RSDO) became the preferred method for acquiring satellites. Notwithstanding, over the past 30 years technology has advanced considerably, and the time is ripe to reconsider modularity in its own right, as enabler of R(sup 2), and as a key element of transformational systems. The MR2 architecture provides a competitive advantage over the old modular approach in its rapid response to market needs that are difficult to predict both from the perspectives of evolving technology, as well as mission and application requirements.
Document ID
20040081112
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Esper, Jaime
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Andary, Jim
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Oberright, John
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
So, Maria
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Wegner, Peter
(Air Force Research Lab. Kirkland AFB, NM, United States)
Hauser, Joe
(Naval Research Lab. Washington, DC, United States)
Date Acquired
September 7, 2013
Publication Date
March 31, 2004
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2004-3002
Report Number: AIAA Paper 2004-3002
Meeting Information
Meeting: AIAA 2nd Responsive Space Conference
Location: El Segundo, CA
Country: United States
Start Date: April 19, 2004
End Date: April 22, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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