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The Importance of Technology Readiness in NASA Earth Venture MissionsThe first set of Venture-class investigations share the characteristic that the technology should be mature and all investigations must use mature technology that has been modeled or demonstrated in a relevant environment (Technology Readiness Level (TRL) >5). Technology Readiness Levels are a systematic metric/measurement system that supports assessments of the maturity of a particular technology and the consistent comparison of maturity between different types of technology. The TRL is used in NASA technology planning. A major step in the level of fidelity of the technology demonstration follows the completion of TRL 5. At TRL 6, a system or subsystem model or prototype must be demonstrated in a relevant environment (ground or space) representative model or prototype system or system, which would go well beyond ad hoc, "patch-cord," or discrete component level breadboarding. These TRL levels are chosen as target objectives for the Program. The challenge for offerors is that they must identify key aspects (uncertainty, multi subsystem complexity, etc) of the TRL estimate that should be properly explained in a submitted proposal. Risk minimization is a key component of the Earth Venture missions. Experiences of prior airborne missions will be shared. The discussion will address aspects of uncertainty and issues surrounding three areas of airborne earth science missions: (1) Aircraft or proposed flight platform -- Expressing the capability of the aircraft in terms of the supporting mission requirements. These issues include airplane performance characteristics (duration, range, altitude, among others) and multiship complexities. (2) Instruments -- Establishing that the instruments have been demonstrated in a relevant environment. Instruments with heritage in prior space missions meet this requirement, as do instruments tested on the ground. Evidence that the instruments have demonstrated the ability to collect data as advertised will be described. The complexity of the integration of multiple subsystems will also be addressed. Issues associated with tailoring the instrument to meet the specific Venture mission objectives must be thoroughly explained and justified. (3) Aircraft/Instrument Integration -- Explicitly defining what development may be required to harden the instrument and integrate the instrument. The challenges associated with this key aspect of major airborne earth science investigations will be presented.
Document ID
20090026592
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wells, James E.
(NASA Langley Research Center Hampton, VA, United States)
Komar, George J.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 24, 2013
Publication Date
July 12, 2009
Subject Category
Technology Utilization And Surface Transportation
Report/Patent Number
LF99-9066
Meeting Information
Meeting: 2009 IEEE International Geoscience and Remote Sensing Symposium
Location: Capetown
Country: South Africa
Start Date: July 12, 2009
End Date: July 17, 2009
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: WBS 144598.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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