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NASA-LLIS-0089
Lessons Learned - Orbiter Structural Integrity
Year: 1992
Abstract: Description of Driving Event:
During launch and ascent, ice from the ET, SRBs, and orbiter may be dislodged by ignition vibroacoustic or aerodynamic forces and impact the orbiter windows or thermal protection system (TPS) with sufficient force to dislodge TPS or damage windows.
During launch and ascent, ice from the ET, SRBs, and orbiter may be dislodged by ignition vibroacoustic or aerodynamic forces and impact the orbiter windows or thermal protection system (TPS) with sufficient force to dislodge TPS or damage windows.
Subject: Flight Equipment
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:20:08Z | |
| date available | 2017-09-04T16:20:08Z | |
| date copyright | 06/15/1992 | |
| date issued | 1992 | |
| identifier other | TJYCQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/83543 | |
| description abstract | Description of Driving Event: During launch and ascent, ice from the ET, SRBs, and orbiter may be dislodged by ignition vibroacoustic or aerodynamic forces and impact the orbiter windows or thermal protection system (TPS) with sufficient force to dislodge TPS or damage windows. | |
| language | English | |
| title | NASA-LLIS-0089 | num |
| title | Lessons Learned - Orbiter Structural Integrity | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Flight Equipment | |
| subject keywords | Flight Operations | |
| subject keywords | Launch Process | |
| subject keywords | Launch Vehicle | |
| subject keywords | Parts Materials & Processes |