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NASA-LLIS-1864
Lessons Learned - External filter needed to achieve low EMI from TWTA
Year: 2008
Abstract: Abstract:
The Lunar Reconnaissance Orbiter required lower levels of Electromagnetic Interference (EMI) than usual to avoid causing sensitive components to malfunction. It was found necessary to use an external filter between the bus and the EPC of the TWTA to obtain the needed level of EMI.
The Lunar Reconnaissance Orbiter required lower levels of Electromagnetic Interference (EMI) than usual to avoid causing sensitive components to malfunction. It was found necessary to use an external filter between the bus and the EPC of the TWTA to obtain the needed level of EMI.
Subject: Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:39:00Z | |
| date available | 2017-09-04T18:39:00Z | |
| date copyright | 09/26/2008 | |
| date issued | 2008 | |
| identifier other | JQXCQCAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/220647 | |
| description abstract | Abstract: The Lunar Reconnaissance Orbiter required lower levels of Electromagnetic Interference (EMI) than usual to avoid causing sensitive components to malfunction. It was found necessary to use an external filter between the bus and the EPC of the TWTA to obtain the needed level of EMI. | |
| language | English | |
| title | NASA-LLIS-1864 | num |
| title | Lessons Learned - External filter needed to achieve low EMI from TWTA | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2008 | |
| contenttype | fulltext | |
| subject keywords | Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments | |
| subject keywords | Integration and Testing |