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Accession Number:
AD0904921
Title:
Shell 405 Catalyst Improvement Substrate Evaluation
Corporate Author:
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
Report Date:
1972-07-01
Abstract:
Fourteen hydrazine catalyst samples on five different substrates provided by Shell Development Company were evaluated in an altitude test chamber. The samples were test fired to determine cold-start life in nominal 5- pound-thrust engines. The new substrates were compared against the standard RA-1 alumina substrate.
Descriptive Note:
Technical rept. 1 Jul 1970-1 Apr 1971 on Phase 1
Pages:
0064
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
2.07MB
