درباره ما
NASA-LLIS-0547
Lessons Learned – Requirement for Stalled-Rotor Power in Worst-Case Thermal Analysis
Year: 1996
Abstract: Description of Driving Event:
On the MIDAS project, thermal analysis for the Shuttle locker payload was performed without the fan in the locked rotor condition (maximum heat dissipation).
On the MIDAS project, thermal analysis for the Shuttle locker payload was performed without the fan in the locked rotor condition (maximum heat dissipation).
Subject: Hardware
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:03:47Z | |
| date available | 2017-09-04T15:03:47Z | |
| date copyright | 06/01/1996 | |
| date issued | 1996 | |
| identifier other | KXBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/1029 | |
| description abstract | Description of Driving Event: On the MIDAS project, thermal analysis for the Shuttle locker payload was performed without the fan in the locked rotor condition (maximum heat dissipation). | |
| language | English | |
| title | NASA-LLIS-0547 | num |
| title | Lessons Learned – Requirement for Stalled-Rotor Power in Worst-Case Thermal Analysis | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
| contenttype | fulltext | |
| subject keywords | Hardware | |
| subject keywords | Test & Verification |