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NASA-LLIS-1512
Lessons Learned - Quench Module Insert (QMI) Furnace Type C Thermocouple (TC) Assembly and Testing Lessons Learned
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:48:47Z | |
| date available | 2017-09-04T17:48:47Z | |
| date copyright | 01/01/2005 | |
| date issued | 2005 | |
| identifier other | ERWEQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/171903 | |
| description abstract | Abstract: The QMI furnace required custom-designed Type C Thermocouples (TC) to meet the scientific requirements for the hardware. In implementing the custom requirement set and associated verification testing for these TCs notable anomalies/problems were encountered in two areas. The primary problem was the discovery of contamination (mostly Carbon deposits) on the inner surfaces of the TC that led to acceptance test failures. A secondary problem was caused by attempting to maximize the TC wire size yet limiting the overall TC sheath diameter leading to assembly problems of each TC. | |
| language | English | |
| title | NASA-LLIS-1512 | num |
| title | Lessons Learned - Quench Module Insert (QMI) Furnace Type C Thermocouple (TC) Assembly and Testing Lessons Learned | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2005 | |
| contenttype | fulltext | |
| subject keywords | Independent Verification and Validation | |
| subject keywords | Program and Project Management | |
| subject keywords | Research & Development | |
| subject keywords | Risk Management/Assessment | |
| subject keywords | Spacecraft | |
| subject keywords | Test & Verification |
