Accession Number : AD0506155
Title : Advanced Storable Z((ClF5/MMH))ZACS Propulsion.
Descriptive Note : Technical rept. Jul 67-Mar 69 on Phase 1,
Corporate Author : AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CALIF
Personal Author(s) : Shantz,Dennis A. ; Butler,Patrick T.
Report Date : AUG 1969
Pagination or Media Count : 145
Abstract : Phase I results include a detailed description of the facility buildup for sea-level testing with ClF5/MMH. The description encompasses the support system, run system, instrumentation, and scrubbers used for disposal of engine exhaust products and liquid chlorine pentafluoride. Four injection techniques were evaluated: splash plate, triplet, doublet, and Hiperthin. These injectors were tested with workhorse copper thrust chambers to determine injector combustion efficiency and the optimum characteristic length for a flight-weight chamber.
Descriptors : (*STORABLE ROCKET PROPELLANTS, *LIQUID PROPELLANT ROCKET ENGINES), PROPELLANT TANKS, EXHAUST GASES, COMBUSTION CHAMBERS, VALVES, THRUST (U) *CHLORINE COMPOUNDS, *FUEL INJECTORS, ATTITUDE CONTROL SYSTEMS, COPPER, BIPROPELLANTS, LIQUID ROCKET OXIDIZERS, METHYL HYDRAZINES, *FLUORIDES, METAL PLATES, FLUORINATION, TUNGSTEN COMPOUNDS, CARBIDES
Subject Categories : Liquid Propellant Rocket Engines
Liquid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE