درباره ما
NASA-LLIS-2057
Lessons Learned – The Vapor Deposited Aluminum (VDA) Coating Process Can Affect Payload Performance
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:13:35Z | |
| date available | 2017-09-04T16:13:35Z | |
| date copyright | 08/27/2009 | |
| date issued | 2009 | |
| identifier other | SRYCQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/76844 | |
| description abstract | Abstract: Vapor deposited aluminum (VDA) coating, performed according to specification on the OSTM/ Jason-2 AMR reflector, caused discontinuities that required rework using a modified VDA process. VDA should not be considered an "off-the-shelf" process. Evaluate any requirement to perform surface roughening prior to VDA coating, and require an adequate margin in the coating thickness. | |
| language | English | |
| title | NASA-LLIS-2057 | num |
| title | Lessons Learned – The Vapor Deposited Aluminum (VDA) Coating Process Can Affect Payload Performance | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2009 | |
| contenttype | fulltext | |
| subject keywords | Additional Categories.Flight Equipment | |
| subject keywords | Additional Categories.Hardware | |
| subject keywords | Additional Categories.Parts | |
| subject keywords | Materials | |
| subject keywords | & Processes | |
| subject keywords | Additional Categories.Payloads | |
| subject keywords | Additional Categories.Spacecraft | |
| subject keywords | Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments | |
| subject keywords | Manufacturing and Assembly | |
| subject keywords | Systems Engineering and Analysis.Engineering design and project processes and standards |
