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Increasing Small Satellite Reliability- A Public-Private InitiativeAt present, CubeSat components and buses are generally not appropriate for missions where significant risk of failure, or the inability to quantify risk or confidence, is acceptable. However, in the future we anticipate that CubeSats will be used for missions requiring reliability of 1-3 years for Earth-observing missions and even longer for Planetary, Heliophysics, and Astrophysics missions. Their growing potential utility is driving an interagency effort to improve and quantify CubeSat reliability, and more generally, small satellite mission risk. The Small Satellite Reliability Initiative (SSRI)—an ongoing activity with broad collaborative participation from civil, DoD, and commercial space systems providers and stakeholders—targets this challenge. The Initiative seeks to define implementable and broadly-accepted approaches to achieve reliability and acceptable risk postures associated with several SmallSat mission risk classes—from “do no harm” missions, to those associated with missions whose failure would result in loss or delay of key national objectives. These approaches will maintain, to the extent practical, cost efficiencies associated with small satellite missions and consider constraints associated with supply chain elements, as appropriate. The SSRI addresses this challenge from two architectural levels—the mission- or system-level, and the component- or subsystem-level. The mission- or system-level scope targets assessment approaches that are efficient and effective, with mitigation strategies that facilitate resiliency to mission or system anomalies while the component- or subsystem-level scope addresses the challenge at lower architectural levels. The initiative does not limit strategies and approaches to proven and traditional methodologies, but is focused on fomenting thought on novel and innovative solutions. This paper discusses the genesis of and drivers for this initiative, how the public-private collaboration is being executed, findings and recommendations derived to date, and next steps towards broadening small satellite mission potential.
Document ID
20180002864
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Johnson, Michael A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Beauchamp, Patricia
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Schone, Harald
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sheldon, Doug
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Fuhrman, Linda
(Massachusetts Inst. of Tech. Lexington, MA, United States)
Sullivan, Erica
(Los Alamos National Lab. NM, United States)
Fairbanks, Tom
(Los Alamos National Lab. NM, United States)
Moe, Miquel
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Leitner, Jesse
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
May 16, 2018
Publication Date
August 5, 2017
Subject Category
Astronautics (General)
Report/Patent Number
GSFC-E-DAA-TN45264
Report Number: GSFC-E-DAA-TN45264
Meeting Information
Meeting: Small Satellite Conference
Location: Logan, Utah
Country: United States
Start Date: August 5, 2017
End Date: August 10, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, Utah State Univ.
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
SmallSat
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