Weight-saving through use of beryllium- aluminum alloys for Saturn-type vehicle structures Final report, 24 Apr. 1965 - 24 Mar. 1966
Weight saving through use of beryllium-aluminum alloys for Saturn-type vehicle structures
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Weight saving through use of beryllium-aluminum alloys for Saturn-type vehicle structures
Lightweight beryllium-aluminum alloys for Saturn launch vehicles
Orientation effect on friction characteristics of single crystal beryllium in vacuum
Rod and sheet metal fabrication of beryllium alloys for spacecraft structures
Ductility and production techniques of cross rolled beryllium sheet
Axially loaded cylindrical structures analyzed for optimum weight construction consistent with cost constraint, emphasizing beryllium-aluminum alloys
Fabrication of beryllium test sheet for structural applications
Metal removal techniques for beryllium in spacecraft structure application
Forming processes for fabrication of beryllium aerospace vehicle structures
Metallurgical evaluation of beryllium powdered metal, and electron microscope studies of agglomerate particle sizes
Pressure drop method for determining chemical kinetics of fluorination of beryllium
Room temperature microstrain behavior of zone- refined single crystal beryllium examined as function of prestrain
Influence of grain-size purity relation beryllium fabrication and resulting mechanical properties
Gas pressure bonding for hot isostatic pressing of beryllium powder into complex shapes
Thin self-supporting beryllium foils preparation for use as atomic and molecular ion beam targets
TREAT microreactor Experiment Cell (T-REXC). This facility will provide a test bed for microreactor developers to perform demonstration projects and critical experiments in an expedited manner. In addition to other systems, structures, and components (SSCs), T-REXC will provide beryllium oxide (BeO) reflector components that T-REXC users can incorporate into their equipment installation. This specification details supplier requirements associated with these BeO components.
In this work, we have applied the Naval Research Laboratory Tight-binding (NRL-TB) Method to the hcp alkaline-earth metal Beryllium. This approach consists of fitting to energy band and total energy data generated by the Linearized Augmented Plane Wave (LAPW) for the fcc, bcc, sc, and hcp structures as a function of volume. First, we found that using the Generalized Gradient Approximation (GGA) for the input data secures a better agreement to experimental volumes than the LDA. Second, we found that including small volumes to the fit is needed to get TB parameters that are transferable enough to successfully predict the energies of structures that were not fitted, and to perform molecular dynamics (MD) simulations. The non-orthogonal Hamiltonian obtained, is successful in correctly predicting the hcp lattice as the ground state of Be and finding eight other structures, that were not fitted to LAPW, positioned at higher energies. In addition, the NRL-TB produces accurate energy bands, densities of states, elastic constants, the Bain path and several quantities derived from MD simulations.
In this work, chemical vapor deposited SiC single crystal and polycrystals were exposed to a static beryllium-bearing molten fluoride salt, 2LiF–BeF 2 for 500 and 1000 h at 750 °C. Overall, the single crystal and polycrystalline SiC materials experienced slight weight loss and nominal surface etching regardless of the material type. Localized pitting and nonuniform Si removal from surface regions were associated with trace metal impurities and oxygen. Cross-sectional observation revealed minimal subsurface changes in the microstructure. The corrosion damage processes were similar to those reported for molten LiF–KF–NaF salt with trace impurities, indicating that the impurities significantly affect SiC corrosion.