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

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

2.07MB