ASD Technical Report, Numéro 63,Partie 635Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963 |
Table des matières
INTRODUCTION | 1 |
DEPOSITION OF COATINGS | 35 |
COMPATIBILITY OF THO₂ WITH BORIDES | 46 |
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A. F. Rosenberg Aeronautical Systems Division argon available boride samples BeO tubes boride rods borides by CO2 BORIDES BY PYROHYDROLYSIS cm/sec COATING BORIDES commercial samples examined commercially available boride COMPATIBILITY WITH BORIDES complicated by slow computed cosh cosh qa dense impervious layers deposit dense impervious diffusion coefficient diffusion equations eerfc END OF FORMAT enrichment Equation I-117 error essentially unsuccessful Evendale exact experiment FORTRAN H. S. Edwards heated hydrogen isotope J. T. Bittel Laplace transform LIMITED VOLUME mass spectrometer Materials and Propulsion METAL HALIDES moles Mt/M ND ND ND percent plasma torch Propulsion Operation pure borides PYROHYDROLYSIS OF METAL pyrohydrolysis of ThC14 ranged from 6.8 rate constant reacted with graphite ROOT samples also reacted selected solid borides self-diffusion of oxygen solution spheres surface reaction susceptor tanh temperatures above 2400°C ThC14 were essentially ThO2 thoria TiB2 transform values Wright-Patterson AFB WRITE OUTPUT TAPE ZrB2