| タイトル | CFM technologies for space transportation: Multipurpose hydrogen testbed system definition and tank procurement |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940008354 |
| 著者（英） | Kiefel, E. R.; Fox, E. C.; Mcintosh, G. L.; Wakefield, M. E.; Sharpe, J. B.; Sheahan, D. R. |
| 著者所属（英） | Martin Marietta Corp. |
| 発行日 | 1993-07-01 |
| 言語 | eng |
| 内容記述 | The development of a test bed tank and system for evaluating cryogenic fluid management technologies in a simulated upper stage liquid hydrogen tank is covered. The tank is 10 ft long and is 10 ft in diameter, and is an ASME certified tank constructed of 5083 aluminum. The tank is insulated with a combination of sprayed on foam insulation, covered by 45 layers of double aluminized mylar separated by dacron net. The mylar is applied by a continuous wrap system adapted from commercial applications, and incorporates variable spacing between the mylar to provide more space between those layers having a high delta temperature, which minimizes heat leak. It also incorporates a unique venting system which uses fewer large holes in the mylar rather than the multitude of small holes used conventionally. This significantly reduces radiation heat transfer. The test bed consists of an existing vacuum chamber at MSFC, the test bed tank and its thermal control system, and a thermal shroud (which may be heated) surrounding the tank. Provisions are made in the tank and chamber for inclusion of a variety of cryogenic fluid management experiments. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 94N12827
NASA-CR-194355
NAS 1.26:194355 |
| 権利 | No Copyright |
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