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Proceedings Paper

Space flight requirements for fiber optic components: qualification testing and lessons learned
Author(s): Melanie N. Ott; Xiaodan Jin; Richard Chuska; Patricia Friedberg; Mary Malenab; Adam Matuszeski
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Paper Abstract

"Qualification" of fiber optic components holds a very different meaning than it did ten years ago. In the past, qualification meant extensive prolonged testing and screening that led to a programmatic method of reliability assurance. For space flight programs today, the combination of using higher performance commercial technology, with shorter development schedules and tighter mission budgets makes long term testing and reliability characterization unfeasible. In many cases space flight missions will be using technology within years of its development and an example of this is fiber laser technology. Although the technology itself is not a new product the components that comprise a fiber laser system change frequently as processes and packaging changes occur. Once a process or the materials for manufacturing a component change, even the data that existed on its predecessor can no longer provide assurance on the newer version. In order to assure reliability during a space flight mission, the component engineer must understand the requirements of the space flight environment as well as the physics of failure of the components themselves. This can be incorporated into an efficient and effective testing plan that "qualifies" a component to specific criteria defined by the program given the mission requirements and the component limitations. This requires interaction at the very initial stages of design between the system design engineer, mechanical engineer, subsystem engineer and the component hardware engineer. Although this is the desired interaction what typically occurs is that the subsystem engineer asks the components or development engineers to meet difficult requirements without knowledge of the current industry situation or the lack of qualification data. This is then passed on to the vendor who can provide little help with such a harsh set of requirements due to high cost of testing for space flight environments. This presentation is designed to guide the engineers of design, development and components, and vendors of commercial components with how to make an efficient and effective qualification test plan with some basic generic information about many space flight requirements. Issues related to the physics of failure, acceptance criteria and lessons learned will also be discussed to assist with understanding how to approach a space flight mission in an ever changing commercial photonics industry.`

Paper Details

Date Published: 21 April 2006
PDF: 15 pages
Proc. SPIE 6193, Reliability of Optical Fiber Components, Devices, Systems, and Networks III, 619309 (21 April 2006); doi: 10.1117/12.669880
Show Author Affiliations
Melanie N. Ott, NASA Goddard Space Flight Ctr. (United States)
Xiaodan Jin, QSS Group Inc. (United States)
Richard Chuska, MEI (United States)
Patricia Friedberg, NASA Goddard Space Flight Ctr. (United States)
Mary Malenab, QSS Group Inc. (United States)
Adam Matuszeski, NASA Goddard Space Flight Ctr. (United States)


Published in SPIE Proceedings Vol. 6193:
Reliability of Optical Fiber Components, Devices, Systems, and Networks III
Hans G. Limberger; M. John Matthewson, Editor(s)

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