Shell 405 Catalyst Improvement Substrate Evaluation
Technical rept. 1 Jul 1970-1 Apr 1971 on Phase 1
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
Pagination or Media Count:
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.
- Inorganic Chemistry
- Liquid Propellant Rocket Engines