LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD

Published date

01-01-2016

Publisher

National Aeronautics and Space Administration

DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. REQUIREMENTS
APPENDIX
A - Requirements Compliance Matrix
B - References

Specifies requirements relative to various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere and standard practices to eliminate or mitigate such reactions.

DevelopmentNote	Supersedes NASA STD 4005(INT). (07/2007)
DocumentType	Standard
PublisherName	National Aeronautics and Space Administration
Status	Current
Supersedes	NASA STD 4005(INT) : 2006

NASA HDBK 4006 : 2007	LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN HANDBOOK
NASA STD 4003 : 2013	ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
BS ISO 17851:2016	Space systems. Space environment simulation for material tests. General principles and criteria
ISO 11221:2011	Space systems Space solar panels Spacecraft charging induced electrostatic discharge test methods
NASA HDBK 4002 : 2011	MITIGATING IN-SPACE CHARGING EFFECTS - A GUIDELINE
15/30281598 DC : 0	BS ISO 17851 - SPACE SYSTEMS - SPACE ENVIRONMENT SIMULATION FOR MATERIAL TESTS - GENERAL PRINCIPLES AND CRITERIA
09/30197011 DC : 0	BS ISO 11221- SPACE SYSTEMS - SPACE SOLAR PANELS - SPACECRAFT CHARGING INDUCED ELECTROSTATIC DISCHARGE TEST MATERIALS
BS ISO 11221:2011	Space systems. Space solar panels. Spacecraft charging induced electrostatic discharge test methods

NASA HDBK 4006 : 2007	LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN HANDBOOK
AIAA S 115 : 2013(R2017)	LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD REQUIREMENT AND ASSOCIATED HANDBOOK