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