| タイトル | Brazing of beryllium for structural applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730013693 |
| 著者（英） | Vogan, J. W. |
| 発行日 | 1972-01-01 |
| 言語 | eng |
| 内容記述 | Progress made in fabricating a beryllium compression tube structure and a stiffened beryllium panel. The compression tube was 7.6cm in diameter and 30.5cm long with titanium end fittings. The panel was 203cm long and stiffened with longitudinal stringers. Both units were assembled by brazing with BAg-18 braze alloy. The detail parts were fabricated by hot forming 0.305cm beryllium sheet and the brazing parameters established. |
| NASA分類 | MACHINE ELEMENTS AND PROCESSES |
| レポートNO | 73N22420
NASA-CR-124245
SOLAR-RDR-1723-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199436 |
