| タイトル | Postflight hardware evaluation 360T025 (RSRM-25, STS-46) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930021428 |
| 著者（英） | Morgan, Ferral |
| 著者所属（英） | Thiokol Corp. |
| 発行日 | 1993-03-01 |
| 言語 | eng |
| 内容記述 | The final report for the Clearfield disassembly evaluation and a continuation of the KSC postflight assessment for the 360T025 (STS-46) Redesign Solid Rocket Motor (RSRM) flight set is presented. All observed hardware conditions were documented on PFOR's and are included in Appendices A through C. Appendices D and E contain the measurements and safety factor data for the nozzle and insulation components. Along with the KSC Ten-Day Postflight Hardware Evaluation Report (TWR-60687), a summary of the 360T025 hardware evaluation is provided. The as-flown hardware configuration is documented in TWR-60470. Disassembly evaluation photograph numbers are logged in TWA-1986. The 360T025 flight set disassembly evaluations described were performed at the RSRM Refurbishment Facility in Clearfield, Utah. The final factory joint demate occurred on 16 Mar. 1993. Detailed evaluations were performed in accordance with the Clearfield PEEP, TWR-50051, Revision A. All observations were compared against limits that are also defined in the PEEP. These limits outline the criteria for categorizing the observations as acceptable, reportable, or critical. Hardware conditions that were unexpected and/or determined to be reportable or critical were evaluated by the applicable CPT and tracked through the PFAR system. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 93N30617
NASA-CR-192562
NAS 1.26:192562
TWR-60699 |
| 権利 | No Copyright |
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