Accession Number : AD0435834
Title : FEASIBILITY DEMONSTRATION OF A TRANSPIRATION COOLED NOZZLE SYSTEM.
Descriptive Note : Interim rept. no. 3, 15 Dec 63-14 Mar 64.
Corporate Author : TRW INC CLEVELAND OHIO
Report Date : 14 Mar 1964
Pagination or Media Count : 49
Abstract : The design, analysis, and fabrication is presented for a porous-tungsten transpiration cooled, test module. Specific accomplishments included the following: the design and analysis for the first throat module test was completed, including verification of the joining method selected, fabrication of the module components has been completed and final assembly has been initiated, simulated test runs using liquid NH3 have been made to verify cooling system operation, and bench tests to verify pressure shock loading, infiltrated graphite performance, hydrogen-tantalum reactivity, and cooling effectivity were completed. (Author)
Descriptors : *ROCKET NOZZLES , SWEAT COOLING , TUNGSTEN , POROUS METALS , HEAT TRANSFER , SOLID PROPELLANT ROCKET ENGINES , FEASIBILITY STUDIES , NOZZLE INSERTS , ELECTRON BEAMS , WELDING , TANTALUM , GRAPHITE , STEEL , TEMPERATURE , AMMONIA , RINGS , NITROGEN , EROSION , PERMEABILITY
Distribution Statement : APPROVED FOR PUBLIC RELEASE