Accession Number : AD0373137
Title : PERFORMANCE CHARACTERISTICS OF A CRYOGENIC TRIPROPELLANT SYSTEM.
Descriptive Note : Quarterly progress rept. no. 5, 1 Mar-31 May 66,
Corporate Author : UNITED AIRCRAFT CORP EAST HARTFORD CONN RESEARCH LABS
Personal Author(s) : Miller ,Charles R. ; McFarlin ,David J. ; Sadowski,Thomas J.
Report Date : JUN 1966
Pagination or Media Count : 35
Abstract : An investigation is being conducted to determine the performance characteristics of a cryogenic tripropellant system in small-scale thrust chambers. This report summarizes the work performed during the period March 1 through May 31, 1966.
Descriptors : (*CRYOGENIC PROPELLANTS, PERFORMANCE(ENGINEERING)), EXHAUST NOZZLES, CAPTIVE TESTS, TEST EQUIPMENT, THRUST (U) BERYLLIUM, OXYGEN, HYDROGEN, ROCKET ENGINES, PYROLYSIS, COMBUSTION CHAMBERS, ALUMINUM, ROCKET PROPELLANT GRAINS, FUELS
Subject Categories : Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE