Operation of hydrodynamic journal bearings in sodium at temperatures to 800 deg F and speeds to 12000 rpm
Operation of hydrodynamic journal bearings in liquid sodium at high temperatures and high speeds
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Operation of hydrodynamic journal bearings in liquid sodium at high temperatures and high speeds
Two-phase flow and material attrition problems for Rankine cycle liquid metal power plants
Effect of drilled holes on notch toughness of iron alloys, noting impact and slow bending testing, notch toughness improvement, etc
Design calculations and materials test data for planetary entry ringsail parachute
Beam-plasma interactions, cyclotron harmonic instabilities, harmonic generation in beam-plasma system, relativistic electron beam studies, and materials tests
High purity dielectric materials tested in capacitors at high temperatures
Data concerning chemical-physical properties of materials tested for spacecraft external coating
Pedestal-type calorimeter measures gamma-ray heating rates from 0.5 to 7.0 watts per gram of aluminum. Nuclear heating rate is a function of cylinder temperature change, measured by four chromel-alumel thermocouples attached to the calorimeter, and known thermoconductivity of the tested material.
Information is given regarding experimental heat-transfer data compiled for the turbulent flow of hydrogen within straight, electrically heated, round cross section tubes. Tube materials, test conditions, parameters studied, and generalized conclusions are presented.
Composite materials testing for fire resistant wall structures for expandable manned space structures
Composite materials tests for expandable manned space structures including flammability, micrometeoroid impact, thermal shock, and tear, puncture, and fungus resistance
Composite window permitting visual or photographic observation and IR irradiation of test materials in ultrahigh vacuum system
Flammability test chamber for testing materials in certain predetermined environments
Hermetic sealing device for ends of tubular bodies during materials testing operations
This study was to experimentally evaluate and mathematically model the performance of phase change thermal control devices containing high thermal conductivity metal matrices. Three aluminum honeycomb filters were evaluated at five different heat flux levels using n-oct-adecane as the test material. The system was mathematically modeled by approximating the partial differential equations with a three-dimensional implicit alternating direction technique. The mathematical model predicts the system quite well. All of the phase change times are predicted. The heating of solid phase is predicted exactly while there is some variation between theoretical and experimental results in the liquid phase. This variation in the liquid phase could be accounted for by the fact that there are some heat losses in the cell and there could be some convection in the experimental system.
Holography and optical filtering techniques for structural analysis, material tests, and astronomical observation - conference
The heat transfer characteristics of various materials used for the thermal insulation of spacecraft are discussed. Techniques for conducting thermal performance analysis, structural performance analysis, and dynamic analysis are described. Processes for producing and finishing the materials are explained. The methods for determining reliability, system safety, materials tests, and design effectiveness are explained.
The proceedings of a conference on NASA Structural Analysis (NASTRAN) to analyze the experiences of users of the program are presented. The subjects discussed include the following: (1) statics and buckling, (2) vibrations and dynamics, (3) substructing, (4) new capability, (5) user's experience, and (6) system experience. Specific applications of NASTRAN to spacecraft, aircraft, nuclear power plants, and materials tests are reported.