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Integrated Technology Assessment Center (ITAC) UpdateThe Integrated Technology Assessment Center (ITAC) has developed a flexible systems analysis framework to identify long-term technology needs, quantify payoffs for technology investments, and assess the progress of ASTP-sponsored technology programs in the hypersonics area. For this, ITAC has assembled an experienced team representing a broad sector of the aerospace community and developed a systematic assessment process complete with supporting tools. Concepts for transportation systems are selected based on relevance to the ASTP and integrated concept models (ICM) of these concepts are developed. Key technologies of interest are identified and projections are made of their characteristics with respect to their impacts on key aspects of the specific concepts of interest. Both the models and technology projections are then fed into the ITAC's probabilistic systems analysis framework in ModelCenter. This framework permits rapid sensitivity analysis, single point design assessment, and a full probabilistic assessment of each concept with respect to both embedded and enhancing technologies. Probabilistic outputs are weighed against metrics of interest to ASTP using a multivariate decision making process to provide inputs for technology prioritization within the ASTP. ITAC program is currently finishing the assessment of a two-stage-to-orbit (TSTO), rocket-based combined cycle (RBCC) concept and a TSTO turbine-based combined cycle (TBCC) concept developed by the team with inputs from NASA. A baseline all rocket TSTO concept is also being developed for comparison. Boeing has recently submitted a performance model for their Flexible Aerospace System Solution for Tomorrow (FASST) concept and the ISAT program will provide inputs for a single-stage-to-orbit (SSTO) TBCC based concept in the near-term. Both of these latter concepts will be analyzed within the ITAC framework over the summer. This paper provides a status update of the ITAC program.
Document ID
20020091933
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Taylor, J. L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Neely, M. A.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Curran, F. M.
(Science Applications International Corp. Huntsville, AL United States)
Christensen, E. R.
(Science Applications International Corp. Huntsville, AL United States)
Escher, D.
(Science Applications International Corp. Huntsville, AL United States)
Lovell, N.
(Science Applications International Corp. Huntsville, AL United States)
Morris, Charles
Date Acquired
September 7, 2013
Publication Date
July 10, 2002
Subject Category
Documentation And Information Science
Report/Patent Number
AIAA Paper 2002-3550
Meeting Information
Meeting: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
CONTRACT_GRANT: NASA Order H-32738-D
Distribution Limits
Public
Copyright
Public Use Permitted.
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