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Cost Estimate for Molybdenum and Tantalum Refractory Metal Alloy Flow Circuit ConceptsThe Early Flight Fission-Test Facilities (EFF-TF) team at NASA Marshall Space Flight Center (MSFC) has been tasked by the Naval Reactors Prime Contract Team (NRPCT) to provide a cost and delivery rough order of magnitude estimate for a refractory metal-based lithium (Li) flow circuit. The design is based on the stainless steel Li flow circuit that is currently being assembled for an NRPCT task underway at the EFF-TF. While geometrically the flow circuit is not representative of a final flight prototype, knowledge has been gained to quantify (time and cost) the materials, manufacturing, fabrication, assembly, and operations to produce a testable configuration. This Technical Memorandum (TM) also identifies the following key issues that need to be addressed by the fabrication process: Alloy selection and forming, cost and availability, welding, bending, machining, assembly, and instrumentation. Several candidate materials were identified by NRPCT including molybdenum (Mo) alloy (Mo-47.5 %Re), tantalum (Ta) alloys (T-111, ASTAR-811C), and niobium (Nb) alloy (Nb-1 %Zr). This TM is focused only on the Mo and Ta alloys, since they are of higher concern to the ongoing effort. The initial estimate to complete a Mo-47%Re system ready for testing is =$9,000k over a period of 30 mo. The initial estimate to complete a T-111 or ASTAR-811C system ready for testing is =$12,000k over a period of 36 mo.
Document ID
20100021082
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Hickman, Robert R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Martin, James J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schmidt, George R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Godfroy, Thomas J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bryhan, A.J.
(Minimal Technology, Inc. San Jose, CA, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M-1280
NASA/TM-2010-216431
Distribution Limits
Public
Copyright
Public Use Permitted.
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