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Technology & Innovation Management Course - Session 2

Technology & innovation Management Course - Session 2

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Session 2 of the Technology & Innovation Management Course. Content: contextual market segmentation, jobs to be done, NASA/DOD technology readiness level

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Page 1: Technology & innovation Management Course - Session 2

Technology & Innovation Management Course

-Session 2

Page 2: Technology & innovation Management Course - Session 2

1. Contextual market segmentation (jobs-to-be-done)

2. NASA technology readiness level

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Contextual market segmentation

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Target markets are not about demographics, sociographics, geographic.

Contextual market segmentation

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Target markets are not about demographics, sociographics, geographic.

Contextual market segmentation

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“People are not buying quarter-inch drills, they buy quarter-inch holes. The drill just happens to be the best means available to get the job done.” 

- Ted Leavitt (Harvard Business School)

Jobs-To-Be-Done

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Jobs-To-Be-Done

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Jobs-To-Be-Done

1. All JTBD are processes;

2. JTBD are followed by JTBD;

3. one JTBD can be fulfilled by multiple solutions;

4. one solution can fulfill multiple JTBD;

5. fall in one or more of the 3 categories:a. functionalb. emotionalc. ancillary

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What are the competitors of a news app?

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What are the competitors of car manufacturer?

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James’ Reading List

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NASA Technology Readiness Level

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL1 Basic principles observed and

reported:

Transition from scientific research to applied research. Essential characteristics and behaviors of systems and architectures. Descriptive tools are mathematical formulations or algorithms.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 2 Technology concept and/or

application formulated:Applied research. Theory and scientific principles are focused on specific application area to define the concept. Characteristics of the application are described. Analytical tools are developed for simulation or analysis of the application.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 3 Analytical and experimental critical

function and/or characteristic proof-of-concept:

Proof of concept validation. Active Research and Development (R&D) is initiated with analytical and laboratory studies. Demonstration of technical feasibility using breadboard or brassboard implementations that are exercised with representative data.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 4 Component/subsystem validation in

laboratory environment:

Standalone prototyping implementation and test.Integration of technology elements. Experiments with full-scale problems or data sets.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 5 System/subsystem/component validation in relevant

environment:Thorough testing of prototyping in representative environment. Basic technology elements integrated with reasonably realistic supporting elements. Prototyping implementations conform to target environment and interfaces.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 6 System/subsystem model or prototyping demonstration in a

relevant end-to-endenvironment (ground or space):

Prototyping implementations on full-scale realistic problems. Partially integrated with existing systems. Limited documentation ava i lab le . Eng ineer ing feas ib i l i t y fu l l y demonstrated in actual system application.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 7 System prototyping demonstration in an operational environment (ground or space):

System prototyping demonstration in operational environment. System is at or near scale of the operational system, with most functions available for demonstration and test. Well integrated with collateral and ancillary systems. Limited documentation available.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 8 Actual system completed and "mission qualified" through test and

demonstration inan operational environment (ground

or space):End of system development. Fully integrated with operational hardware and software systems. M o s t u s e r d o c u m e n t a t i o n , t r a i n i n g documentation, and maintenance documentation completed. All functionality tested in simulated and operational scenarios. Verification and Validation (V&V) completed.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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TRL 9 Actual system "mission proven" through successful mission

operations (ground or space):Fully integrated with operational hardware/software systems. Actual system has been thoroughly demonstrated and tested in its operational environment. All documentation completed. Successful operational experience. Sustaining engineering support in place.

Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Source: http://esto.nasa.gov/files/trl_definitions.pdf

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Hope you

have NO questions!

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