| タイトル | Performance Evaluation of an Actuator Dust Seal for Lunar Operation |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140009203 |
| 著者（英） | Delgado, Irebert R.; Panko, Scott; Handschuh, Michael; Gaier, James R.; Sechkar, Ed |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2013-09-01 |
| 言語 | eng |
| 内容記述 | Exploration of extraterrestrial surfaces (e.g. moon, Mars, asteroid) will require durable space mechanisms that will survive potentially dusty surface conditions in addition to the hard vacuum and extreme temperatures of space. Baseline tests with lunar simulant were recently completed at NASA GRC on a new Low-Temperature Mechanism (LTM) dust seal for space actuator application. Following are top-level findings of the tests completed to date in vacuum using NU-LHT-2M lunar-highlands simulant. A complete set of findings are found in the conclusions section.Tests were run at approximately 10-7 torr with unidirectional rotational speed of 39 RPM.Initial break-in runs were performed at atmospheric conditions with no simulant. During the break-in runs, the maximum torque observed was 16.7 lbf-in. while the maximum seal outer diameter temperature was 103F. Only 0.4 milligrams of NU-LHT-2M simulant passed through the sealshaft interface in the first 511,000 cycles while under vacuum despite a chip on the secondary sealing surface.Approximately 650,000 of a planned 1,000,000 cycles were completed in vacuum with NU-LHT-2M simulant.Upon test disassembly NU-LHT-2M was found on the secondary sealing surface. |
| NASA分類 | Lunar and Planetary Science and Exploration |
| レポートNO | GRC-E-DAA-TN10013
E-18781
NASA/TM-2013-216587 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/70905 |
