Accession Number : AD0429467


Title :   DEVELOPMENT AND UTILIZATION OF OPTIMUM TECHNIQUES FOR THE FABRICATION OF TITANIUM BORONITRIDE ROCKET NOZZLES.


Descriptive Note : Interim rept. no. 1, 1 Jan-30 June 63,


Corporate Author : CALOROBIC MATERIALS INC PEARL RIVER N Y


Personal Author(s) : Strickman,R


Report Date : Jul 1963


Pagination or Media Count : 24


Abstract : Various test specimens and rocket nozzle inserts were produced of various throat diameters from a material composed principally of titanium diboride, titanium nitride and boron nitride. The scope of this project is to develop optimum techniques for fabricating sound, dense, crackfree specimens and rocket nozzle inserts in specified sizes of the material system - Titanium, Boron, Nitrogen. (Author)


Descriptors :   *ROCKET NOZZLES , MANUFACTURING , REFRACTORY MATERIALS , TITANIUM , BORON COMPOUNDS , NITRIDES , NOZZLE INSERTS , POWDER METALS , TITANIUM COMPOUNDS , TEST EQUIPMENT


Distribution Statement : APPROVED FOR PUBLIC RELEASE