136 research outputs found

    THE NOBLE GAS PERMEABILITY CHARACTERISTICS OF GRAPHITE MATERIALS FOR USE IN GAS-COOLED REACTORS

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    S>The theory of gas permeation through porous materials is reviewed in brief. Experimental data are presented on the permeation of He and the fission product noble gases as a function of pressure, temperature, and time of annealing through various graphite materials of interest for use to contain or hold back volatile fission products in gas-cooled reactors. (auth

    Electro-impulse de-icing testing analysis and design

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    Electro-Impulse De-Icing (EIDI) is a method of ice removal by sharp blows delivered by a transient electromagnetic field. Detailed results are given for studies of the electrodynamic phenomena. Structural dynamic tests and computations are described. Also reported are ten sets of tests at NASA's Icing Research Tunnel and flight tests by NASA and Cessna Aircraft Company. Fabrication of system components are described and illustrated. Fatigue and electromagnetic interference tests are reported. Here, the necessary information for the design of an EIDI system for aircraft is provided

    FISSION PRODUCT ELEMENT YIELDS AND CHARACTERISTICS

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    Studies of thermionic materials for space power applications informal monthly report, sep. 1 - sep. 30, 1963

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    Thermionic materials for space power application - uranium carbide-zirconium carbide fuels and tungsten claddin

    Studies of thermionic materials for space power applications informal monthly report, oct. 1 - oct. 31, 1963

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    Thermionic space power material - isostatic pressing, vapor deposited tungsten, high temperature properties, cesium thermionic cell life testing, and irradiation studie

    Entry, Descent and Landing Systems Analysis Study: Phase 1 Report

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    NASA senior management commissioned the Entry, Descent and Landing Systems Analysis (EDL-SA) Study in 2008 to identify and roadmap the Entry, Descent and Landing (EDL) technology investments that the agency needed to make in order to successfully land large payloads at Mars for both robotic and human-scale missions. This paper summarizes the motivation, approach and top-level results from Year 1 of the study, which focused on landing 10-50 mt on Mars, but also included a trade study of the best advanced parachute design for increasing the landed payloads within the EDL architecture of the Mars Science Laboratory (MSL) missio
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