Name: NASA KSC STD E 0004 : 2008
Brand: NASA

PNEUMATIC AND HYDRAULIC MECHANICAL COMPONENTS, ELECTRICAL DESIGN, STANDARD FOR

Published date

01-01-2008

Publisher

National Aeronautics and Space Administration

1. SCOPE
2. APPLICABLE DOCUMENTS
   2.1 Governmental
   2.2 Non-Governmental
3. DEFINITIONS
4. REQUIREMENTS
   4.1 Electrical Wiring
        4.1.1 Wire Identification Code
        4.1.2 Terminating
        4.1.3 Lacing or Sleeving
        4.1.4 Slack Wiring
        4.1.5 Hookup Wire
        4.1.6 Wire Gage
        4.1.7 Magnetic Wire
   4.2 Solenoid Coils
        4.2.1 Hookup
        4.2.2 Impregnation and Encapsulation
        4.2.3 Sealing
        4.2.4 Operating Voltage Requirements
   4.3 Switching Assemblies
        4.3.1 Makeup and Qualification
        4.3.2 Sealed Units
        4.3.3 Nonsealed Units
        4.3.4 Warning Label
        4.3.5 Current and Voltage Rating
        4.3.6 Voltage Drops
        4.3.7 Switching Assemblies Requiring a Power Source
   4.4 Position Indicators
        4.4.1 Sensor Position Indication
        4.4.2 Sensor Actuation
        4.4.3 Independence of Circuits
        4.4.4 Operating Voltage Requirements
   4.5 Potting Compound
        4.5.1 Material
        4.5.2 Molds
        4.5.3 Coverage
   4.6 Electrical Connectors
        4.6.1 Standard Connectors
        4.6.2 Hermetically Sealed Units
        4.6.3 Connector Insulation
   4.7 Pin Functions
        4.7.1 Single Solenoid With a 2-Pin Connector
        4.7.2 Double Solenoid Valve With a 3-Pin Connector
        4.7.3 Solenoid and Indicator Switch With 4-Pin Connector
        4.7.4 Double Solenoid Valve With a 3-Pin Connector
              for Position Indicator
        4.7.5 Solenoid and Indicator Switch With a 5-Pin
              Connector
        4.7.6 Double Solenoid Valve With a 6-Pin Connector
              for Position Indicator
        4.7.7 Switches (Limit, Indicator, and Others
        4.7.8 Potentiometer-Type Transducers
   4.8 Insulation Resistance
   4.9 External Markings
        4.9.1 Diagrams
        4.9.2 Connector Designations
        4.9.3 Other Markings
   4.10 Testing
   4.11 Documentation
5. QUALITY ASSURANCE PROVISIONS
   5.1 Inspectability
   5.2 Integrity Control
   5.3 Inspections and Tests
   5.4 Contractual Provisions
6. PREPARATION FOR DELIVERY
7. NOTES
   7.1 Intended Use

Describes the requirements applicable to the electrical design of pneumatic and hydraulic mechanical components at the KSC, NASA. Also pertains to those components located support equipment (GSE) where the natural or induced environment is severe and component reliability is essential.

DocumentType	Standard
PublisherName	National Aeronautics and Space Administration
Status	Current

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