Remote observations of Earth from space serve an extraordinarily broad range of purposes, resulting in extraordinary demands on those at the National Aeronautics and Space Administration (NASA), the National Oceanic and Atmospheric Administration (NOAA), and elsewhere who must decide how to execute them. In research, Earth observations promise large volumes of data to a variety of disciplines with differing needs for measurement type, simultaneity, continuity, and long-term instrument stability. Operational needs, such as weather forecasting, add a distinct set of requirements for continual and highly reliable monitoring of global conditions.
The Role of Small Satelites in NASA and NOAA Earth Observation Porgrams confronts these diverse requirements and assesses how they might be met by small satellites. In the past, the preferred architecture for most NASA and NOAA missions was a single large spacecraft platform containing a sophisticated suite of instruments. But the recognition in other areas of space research that cost-effectiveness, flexibility, and robustness may be enhanced by using small spacecraft has raised questions about this philosophy of Earth observation. For example, NASA has already abandoned its original plan for a follow-on series of major platforms in its Earth Observing System.
This study finds that small spacecraft can play an important role in Earth observation programs, providing to this field some of the expected benefits that are normally associated with such programs, such as rapid development and lower individual mission cost. It also identifies some of the programmatic and technical challenges associated with a mission composed of small spacecraft, as well as reasons why more traditional, larger platforms might still be preferred. The reasonable conclusion is that a systems-level examination is required to determine the optimum architecture for a given scientific and/or operational objective. The implied new challenge is for NASA and NOAA to find intra- and interagency planning mechanisms that can achieve the most appropriate and cost-effective balance among their various requirements.
Table of Contents
|2 Core Observational Needs||11-21|
|3 Payload Sensor Characteristics||22-30|
|4 Small Satellite Buses||31-36|
|5 Small Launch Vehicles||37-40|
|6 Small Satellites and Mission Architectures||41-50|
|7 Opportunities and Challenges in Managing Small Satellite Systems||51-57|
|8 Findings and Recommendations||58-66|
|Appendix A: Statement of Task||67-68|
|Appendix B: Effects of Technology on Sensor Size and Design||69-76|
|Appendix C: U.S. Launch Vehicles for Small Satellites||77-81|
|Appendix D: Case Studies||82-89|
|Appendix E: Acronyms and Abbreviations||90-92|
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