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Abstract:
The purpose of this program is to develop two thermal-shock-resistant composite carbide systems that can be reliably used with high-flame-temperature solid rocket propellants. These are: a microcomposite of monocarbide (tantalum, hafnium) and a tantalum-carbide-coated, tantalum carbide/graphite hypereutectic. During this second quarter, the processing variables required to develop the microcomposite structure were established utilizing a hot-press fabrication technique. Work was initiated to develop a tantalum carbide/graphite hypereutectic composite by a fusion and drop casting technique. (Author)
| Description: |
Quarterly rept. no. 2, 1 Oct-31 Dec 66 |
| Pages: |
44 |
| Report Date: |
JAN 1967 |
| Contract Number: |
611, AF0461111608 |
| Report Number: |
0270508 |
Report Unavailable |
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