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Application of Rapid Prototyping to the Investment Casting of Test Hardware (MSFC Center Director's Discretionary Fund Final Report, Project No. 98-08)Investment casting masters of a selected propulsion hardware component, a fuel pump housing, were rapid prototyped on the several processes in-house, along with the new Z-Corp process acquired through this project. Also, tensile samples were prototyped and cast using the same significant parameters. The models were then shelled in-house using a commercial grade zircon-based slurry and stucco technique. Next, the shelled models were fired and cast by our in-house foundry contractor (IITRI), with NASA-23, a commonly used test hardware metal. The cast models are compared by their surface finish and overall appearance (i.e., the occurrence of pitting, warping, etc.), as well as dimensional accuracy.
Document ID
20000073847
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Cooper, K. G.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Wells, D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2000
Subject Category
Engineering (General)
Report/Patent Number
M-983
NASA/TM-2000-210384
NAS 1.15:210384
Report Number: M-983
Report Number: NASA/TM-2000-210384
Report Number: NAS 1.15:210384
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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