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Accession Number:
AD0843084
Title:
Carbides for Solid Propellant Nozzle Systems
Corporate Author:
TRW EQUIPMENT LABS CLEVELAND OH MATERIALS TECHNOLOGY DEPT
Report Date:
1968-10-01
Abstract:
The magnitude of reactivity between Al2O3 and carbide composite rocket nozzle throat materials was assessed by means of laboratory tests. A secondary objective of the program was to establish the validity of the laboratory tests in evaluating material performance. The program included a plasma jet test that measured mechanical and chemical erosion and a static reactivity test to separate the purely chemical effects. A prediction of the performance of the carbide composites in a test firing was made, based on the laboratory tests.
Descriptive Note:
Final technical rept. 1 Oct 1967-30 Jun 1968
Pages:
0045
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
F04611-67-C-0094
File Size:
1.97MB
