| タイトル | Analysis and Design of the NASA Langley Cryogenic Pressure Box |
| 本文（外部サイト） | http://hdl.handle.net/2060/20000011223 |
| 著者（英） | Blackburn, Charles L.; Glass, David E.; Maguire, James F.; Vause, R. Frank; Stevens, Jonathan C.; Driscoll, Glenn C.; Winn, Peter M.; Mason, Brian H. |
| 著者所属（英） | Analytical Services and Materials, Inc. |
| 発行日 | 1999-12-01 |
| 言語 | eng |
| 内容記述 | A cryogenic pressure box was designed and fabricated for use at NASA Langley Research Center (LaRC) to subject 72 in. x 60 in. curved panels to cryogenic temperatures and biaxial tensile loads. The cryogenic pressure box is capable of testing curved panels down to -423 F (20K) with 54 psig maximum pressure on the concave side, and elevated temperatures and atmospheric pressure on the convex surface. The internal surface of the panel is cooled by high pressure helium as that is cooled to -423 F by liquid helium heat exchangers. An array of twelve independently controlled fans circulate the high pressure gaseous helium to provide uniform cooling on the panel surface. The load introduction structure, consisting of four stainless steel load plates and numerous fingers attaching the load plates to the test panel, is designed to introduce loads into the test panel that represent stresses that will he observed in the actual tank structure. The load plates are trace cooled with liquid nitrogen to reduce thermal gradients that may result in bending the load plates, and thus additional stresses in the test panel. The design of the cryogenic systems, load introduction structure, and control system are discussed in this report. |
| NASA分類 | Ground Support Systems and Facilities (Space) |
| レポートNO | NAS 1.26:209822
AS/M-H5-99-01
NASA/CR-1999-209822 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/95470 |
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