EMI/EMC, lightning, and ESD design approach for the Falcon 9 launch vehicle: Part i

IEEE International Symposium on Electromagnetic Compatibility

Volumn , Issue , 2011, Pages 290-294

  Elkman, W ^a   Trinh, J ^a   McCaughey, P ^a   Chen, W ^a  

^a and Navigation Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN APPROACHES; DESIGN PERFORMANCE; DETAILED DESIGN; EMI/EMC; FUNCTIONAL PERFORMANCE; INDUSTRY STANDARDS; SPACE EXPLORATION TECHNOLOGIES; TEST METHOD; TEST REQUIREMENTS;

DESIGN; ELECTROMAGNETIC COMPATIBILITY; ELECTROMAGNETISM; LAUNCH VEHICLES; REGULATORY COMPLIANCE; SPACE FLIGHT; SPACE RESEARCH;

LAUNCHING;

EID: 80054723919     PISSN: 10774076     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ISEMC.2011.6038324     Document Type: Conference Paper

References (8)

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4. 'ANSI Standard for Safe Use of Lasers', ANSI Z136.1-2007, 2007
5. 'STS Electrical Auxiliary Power Unit (EAPU) Corona Design Guideline', JSC-29129, June 2000
6. 'LEO Spacecraft Charging Design Standard', NASA-STD-4005, June 2007
7. 'LEO Spacecraft Charging Design Handbook', NASA-HDBK-4006, June 2007
8. 'Avoiding Problems Caused by S/C On-orbit Internal Charging Effects', NASA-HDBK-4002, Feb 1999.