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  • NASA MSFC STD 1800 : 2008

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    ELECTROSTATIC DISCHARGE (ESD) CONTROL FOR PROPELLANT AND EXPLOSIVE DEVICES

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    Published date:  01-01-2008

    Publisher:  National Aeronautics and Space Administration

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

    1.0 SCOPE
    1.1 Purpose
    1.2 Applicability and Exclusions
    1.3 Tailoring
    2.0 APPLICABLE DOCUMENTS
    3.0 DEFINITIONS
    4.0 GENERAL REQUIREMENTS
    4.1 ESD Control Program
    4.2 Test Program
        4.2.1 Test Program Results
    4.3 ESD Training Program
        4.3.1 ESD Training Documentation
    4.4 Quality Requirements
        4.4.1 Inspection Responsibility
        4.4.2 Internal Quality Records
        4.4.3 Documentation
        4.4.4 ESD Testing
    4.5 Safety Requirements
        4.5.1 Training
        4.5.2 Documentation
    4.6 Audits and Reviews
        4.6.1 Internal Audits
        4.6.2 Government Audits
        4.6.3 Design Reviews
        4.6.4 Program Reviews
    4.7 MSFC On-site Operations
        4.7.1 MSFC Personnel and on-site contractors
        4.7.2 Verification
        4.7.3 Document Approvals
    4.8 Prime Contractor control
    4.9 Subcontractor Control
    5.0 DETAILED REQUIREMENTS
    5.1 Handling, Shipping, and Storage Requirements
        5.1.1 Shipping Container Design
    5.2 Operational Controls
    5.3 Solid Propellant
        5.3.1 Analysis and Tests
        5.3.2 Solid Rocket Motors
        5.3.3 Solid Rocket Assessment
        5.3.4 Hazard Analysis
        5.3.5 Grounding and Bonding
    5.4 Liquid Propellant
        5.4.1 Design Requirements
        5.4.2 Hazard Analysis
        5.4.3 Grounding and Bonding
        5.4.4 Loading
        5,4.5 Storage Tanks
        5.4.6 Ullage Gases
        5.4.7 Composites
    5.5 Explosive Devices
        5.5.1 Testing
        5.5.2 Lead Azide and Lead Styphnate
        5.5.3 Grounding and Bonding
        5.5.4 Storage and Shipment
        5.5.5 Operating Precautions
    APPENDICES
    A APPLICABLE DOCUMENTS
    B ESD TERMS AND DEFINITIONS
    C ESD TRAINING GUIDELINES

    Abstract - (Show below) - (Hide below)

    Establishes requirements for the development of appropriate control measures to provide protection against personnel injury, property damage, and/or mission degradation due to the discharge of electrostatic energy (ESE) and subsequent initiation of propellant or explosive devices (ordnance).

    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)

    NASA MSFC SPEC 3635 : 2012 PYROTECHNIC SYSTEM SPECIFICATION
    NASA KSC STD E 0012 : 2013 FACILITY GROUNDING AND LIGHTNING PROTECTION, STANDARD FOR
    NASA MSFC RQMT 2918 : 2015 REQUIREMENTS FOR ELECTROSTATIC DISCHARGE CONTROL

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

    MIL-PRF-81705 Revision E:2009 Barrier Materials, Flexible, Electrostatic Discharge Protective, Heat-Sealable
    MIL-HDBK-1512 Base Document:1997 ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS
    MIL-HDBK-83578 Base Document:1999 CRITERIA FOR EXPLOSIVE SYSTEMS AND DEVICES USED ON SPACE VEHICLES
    NASA STD 4003 : 2013 ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
    MIL-STD-464 Revision C:2010 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    MIL-DTL-23659 Revision F:2010 Initiators, Electric, General Design Specification for
    NASA KSC STD E 0012 : 2013 FACILITY GROUNDING AND LIGHTNING PROTECTION, STANDARD FOR
    NFPA 70 : 2017 NATIONAL ELECTRICAL CODE
    MIL-STD-1576 Base Document:1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS
    NFPA 77 : 2014 STATIC ELECTRICITY
    AIAA G 095 : 2004 GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS
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