Accession Number : AD0506391

Title :   Injector/Chamber Scaling Evaluation, Facility Checkout.

Descriptive Note : Technical rept.,

Corporate Author : AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CALIF

Personal Author(s) : Powell,Michael F. ; Powell,Patrick W. ; Fleiszar,Mitchell J. , Jr. ; Main,Howard V.

Report Date : MAR 1969

Pagination or Media Count : 74

Abstract : This report describes the results of the checkout test series conducted at the High Thrust Facility. This project, a task under the overall Minimum Cost Design Launch Vehicle Program, will develop low-cost high-performing injectors at 250,000 pounds thrust using N2O4/UDMH propellants and will evaluate their scalability up to the multimillion-pound-thrust class.

Descriptors :   (*FUEL INJECTORS, COMBUSTION CHAMBERS), (*LIQUID PROPELLANT ROCKET ENGINES, FUEL INJECTORS), THRUST, LIQUEFIED GASES, LIQUID ROCKET PROPELLANTS, COST EFFECTIVENESS, HYDROGEN, CRYOGENICS, INSTRUMENTATION, LIQUID ROCKET OXIDIZERS, FLUID FLOW, THERMOCHEMISTRY, THERMAL PROPERTIES, PROPELLANT TANKS (U) NITROGEN OXIDES, PROPELLANT CONTROL, METHYL HYDRAZINES, TETROXIDES, STAINLESS STEEL, NOISE, EXHAUST GASES

Subject Categories : Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE