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                   112                       MEMS and Microstructures in Aerospace Applications



                   TABLE 6.1
                   Technology Readiness Level (TRL) Scale

                   TRL1          Basic principles observed and reported
                   TRL2          Technology concept and application formulated
                   TRL3          Analytical and experimental critical function and/or characteristic proof-of-concept
                   TRL4          Component and/or breadboard validation in laboratory environment
                   TRL5          Component and/or breadboard validation in relevant environment
                   TRL6          System or subsystem model or prototype demonstration in a relevant
                                  environment (ground or space)
                   TRL7          System prototype demonstration in a space environment
                   TRL8          Actual system completed and ‘‘flight qualified’’ through test and
                                  demonstration (ground or flight)
                   TRL9          Actual system ‘‘flight proven’’ through successful mission operations
                   Source: NASA/JPL.






                   concepts are at the low TRL stage, sometimes referred to as the ‘‘technology push’’
                                                                            4
                   stage, with the daunting challenge of having to bridge the ‘‘TRL gap’’ to success-
                   fully transition to the high-TRL space applications or ‘‘technology pull’’ stage. The
                   TRL gap, sometimes referred to as the ‘‘valley of death’’ in the commercial sector,
                   therefore represents an order-of-magnitude increase in effort (and consequently
                   funding) that is required to make the transition to high TRL. The primary reason
                   that most new technologies fail to bridge the TRL gap is that because of their
                   relatively low maturity, they do not have a compelling mission ‘‘pull’’ to drive
                   further system-level development.
                       Another important consideration is that space applications only need compon-
                   ents and systems in relatively minuscule volumes compared to the consumer
                   market. However, the performance requirements for these technologies are no less
                   stringent, and in most cases, much more so than for consumer products. Thus, the
                   system development costs are considerable since a sufficiently large body of
                   laboratory test data has to be generated in order to conclusively demonstrate the
                   reliability of the new technology. Additionally, there is also a more subtle percep-
                   tion barrier to be overcome. This involves the generation of sufficient ‘‘space
                   heritage’’ via actual space flights of the new system. Carried to the extreme, this
                   perception barrier leads to the conundrum that a new technology cannot fly unless it
                   has flown before! NASA has recognized the impact of the space heritage barrier as
                   a major obstacle impeding the infusion of new technologies into its missions. This
                   recognition has led to the setting up of programs such as the New Millennium
                   Program (NMP) that are aimed specifically to provide flight demonstration oppor-
                   tunities for new technologies. These flights, however, are few and far between, and
                   are also generally restricted to technologies that are already at a high level of
                   maturity (TRL 4 and above).




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