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The Need for Technology Maturity of Any Advanced Capability to Achieve Better Life Cycle Cost (LCC)Programs such as space transportation systems are developed and deployed only rarely, and they have long development schedules and large development and life cycle costs (LCC). They have not historically had their LCC predicted well and have only had an effort to control the DDT&E phase of the programs. One of the factors driving the predictability, and thus control, of the LCC of a program is the maturity of the technologies incorporated in the program. If the technologies incorporated are less mature (as measured by their Technology Readiness Level - TRL), then the LCC not only increases but the degree of increase is difficult to predict. Consequently, new programs avoid incorporating technologies unless they are quite mature, generally TRL greater than or equal to 7 (system prototype demonstrated in a space environment) to allow better predictability of the DDT&E phase costs unless there is no alternative. On the other hand, technology development programs rarely develop technologies beyond TRL 6 (system/subsystem model or prototype demonstrated in a relevant environment). Currently the lack of development funds beyond TRL 6 and the major funding required for full scale development leave little or no funding available to prototype TRL 6 concepts so that hardware would be in the ready mode for safe, reliable and cost effective incorporation. The net effect is that each new program either incorporates little new technology or has longer development schedules and costs, and higher LCC, than planned. This paper presents methods to ensure that advanced technologies are incorporated into future programs while providing a greater accuracy of predicting their LCC. One method is having a dedicated organization to develop X-series vehicles or separate prototypes carried on other vehicles. The question of whether such an organization should be independent of NASA and/or have an independent funding source is discussed. Other methods are also discussed. How to make the choice of which technologies to pursue to the prototype level is also discussed since, to achieve better LCC, first the selection of the appropriate technologies.
Document ID
20130012517
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Robinson, John W.
(Boeing Co. Huntington Beach, CA, United States)
Levack, Daniel J. H.
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Rhodes, Russel E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Chen, Timothy T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
August 2, 2009
Subject Category
Economics And Cost Analysis
Report/Patent Number
AIAA Paper 2009-5347
KSC-2009-067
Meeting Information
Meeting: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Denver, CO
Country: United States
Start Date: August 2, 2009
End Date: August 5, 2009
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Electrical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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