| タイトル | Solid Propulsion Systems, Subsystems, and Components Service Life Extension |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120001765 |
| 著者（英） | Hundley, Nedra H.; Jones, Connor |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2011-12-01 |
| 言語 | eng |
| 内容記述 | The service life extension of solid propulsion systems, subsystems, and components will be discussed based on the service life extension of the Space Transportation System Reusable Solid Rocket Motor (RSRM) and Booster Separation Motors (BSM). The RSRM is certified for an age life of five years. In the aftermath of the Columbia accident there were a number of motors that were approaching the end of their five year service life certification. The RSRM Project initiated an assessment to determine if the service life of these motors could be extended. With the advent of the Constellation Program, a flight test was proposed that would utilize one of the RSRMs which had been returned from the launch site due to the expiration of its five year service life certification and twelve surplus Chemical Systems Division BSMs which had exceeded their eight year service life. The RSRM age life tracking philosophy which establishes when the clock starts for age life tracking will be described. The role of the following activities in service life extension will be discussed: subscale testing, accelerated aging, dissecting full scale aged hardware, static testing full scale aged motors, data mining industry data, and using the fleet leader approach. The service life certification and extension of the BSMs will also be presented. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | M11-1080 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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