• NASA HDBK 4002 : 2011

    Current The latest, up-to-date edition.

    MITIGATING IN-SPACE CHARGING EFFECTS - A GUIDELINE

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    Published date:  01-01-2011

    Publisher:  National Aeronautics and Space Administration

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    Table of Contents - (Show below) - (Hide below)

    DOCUMENT HISTORY LOG
    FOREWORD
    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. ACRONYMS, ABBREVIATIONS, AND DEFINITIONS
    4. INTRODUCTION TO PHYSICS OF CHARGING AND DISCHARGING
    5. SPACECRAFT DESIGN GUIDELINES
    6. SPACECRAFT TEST TECHNIQUES
    7. CONTROL AND MONITORING TECHNIQUES
    8. MATERIAL NOTES AND TABLES
    APPENDICES
    A - The Space Environment
    B - Environment, Electron Transport, and Spacecraft Charging
        Computer Codes
    C - Internal Charging Analyses
    D - Test Methods
    E - Voyager SEMCAP Analysis
    F - Simple Approximations: Spacecraft Surface Charging
        Equations
    G - Derivation of Rule Limiting Open Circuit Board Area
    H - Expanded Worst-Case Geosynchronous Earth Environments
        Descriptions
    I - References and Bibliography
    J - Acknowledgements
    K - Contact Information
    Index

    Abstract - (Show below) - (Hide below)

    Proposes to describe conditions under which spacecraft charging might be an issue, generally explain why the problem exists, list typical design solutions, and provide an introduction to the process by which design specifics should be resolved.

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Publisher National Aeronautics and Space Administration
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    BS ISO 14302:2002 Aerospace series. Space systems. Electromagnetic compatibility requirements
    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
    UNI EN 16603-20-06 : 2014 SPACE ENGINEERING - SPACECRAFT CHARGING
    EN 16603-20-06:2014 Space engineering - Spacecraft charging
    I.S. EN 16603-20-06:2014 SPACE ENGINEERING - SPACECRAFT CHARGING
    BS EN 16603-20-06:2014 Space engineering. Spacecraft charging
    15/30281598 DC : 0 BS ISO 17851 - SPACE SYSTEMS - SPACE ENVIRONMENT SIMULATION FOR MATERIAL TESTS - GENERAL PRINCIPLES AND CRITERIA
    ISO 14302:2002 Space systems Electromagnetic compatibility requirements

    Standards Referencing This Book - (Show below) - (Hide below)

    NASA STD 4005 : 2016 LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD
    MIL-STD-883 Revision K:2016 TEST METHOD STANDARD - MICROCIRCUITS
    MIL-STD-1541 Revision A:1987 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS
    NASA HDBK 4006 : 2007 LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN HANDBOOK
    ASTM D 257 : 2014 : REDLINE Standard Test Methods for DC Resistance or Conductance of Insulating Materials
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