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Quench Module Insert Capabilities and Development Test ResultsThe Quench Module Insert is a directional solidification furnace that will operate in the Materials Science Research Rack (MSRR) on the International Space Station. It will provide high thermal gradient and quench capabilities for processing metals and alloys in microgravity. Numerical analyses and breadboard testing conducted to date show that the QMI can produce an axial temperature gradient approaching 150 C per centimeter in a 1 centimeter diameter aluminum sample with a maximum molten sample temperature of 1100 C. Breadboard testing and analysis have also shown that the quench capabilities of the furnace are sufficient to rapidly solidify at least a 5mm axial portion of a 1 centimeter diameter molten aluminum sample in significantly less than the required 2 seconds and prevent significant backmelt. This paper presents the furnace requirements and capabilities and a status of the associated development testing and analyses.
Document ID
20020022714
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Carswell, William E.
(Alliance for Microgravity Materials Science and Applications Huntsville, AL United States)
Crouch, M. R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Farmer, J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Breeding, S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Rose, F.
(Pace and Waite, Inc. Huntsville, AL United States)
Whitaker, Ann F.
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2001-4997
Meeting Information
Meeting: International Space Station Utilization Conference
Location: Cocoa Beach, FL
Country: United States
Start Date: October 15, 2001
Funding Number(s)
CONTRACT_GRANT: NCC8-66
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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