Electromagnetic compatibility design, implementation and test of the SMAP spacecraft to meet stringent L-Band radiated emissions requirements
Chi-Chien Nelson Huang, Ali Ghaneh, Subha Comandur
Abstract
Chi-Chien Nelson Huang, Ali Ghaneh, Subha Comandur
Abstract
This paper describes the electromagnetic compatibility (EMC) requirements on the NASA SMAP mission, the implementation of EMC best practices at various levels of development in system level cabling harnesses and subsystems packaging, and the testing and results of flight hardware at the subsystem and spacecraft system levels.
OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
This paper describes the electromagnetic compatibility (EMC) requirements on the NASA SMAP mission, the implementation of EMC best practices at various levels of development in system level cabling harnesses and subsystems packaging, and the testing and results of flight hardware at the subsystem and spacecraft system levels.
Key concepts: Electromagnetic compatibility, Spacecraft, Compatibility (geochemistry), Systems engineering, Spacecraft design, Electromagnetic environment, Engineering, System testing