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NASA HDBK 4001 : 0

Current

Current

The latest, up-to-date edition.

ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT

FOREWORD
1. SCOPE
   1.1 Scope
   1.2 Purpose
   1.3 Applicability
   1.4 Constraints
2. APPLICABLE DOCUMENTS
   2.1 General
   2.2 Government documents
       2.2.1 Specifications, standards, and handbooks
   2.3 Order of precedence
3. ACRONYMS AND DEFINITIONS
   3.1 Acronyms used in this handbook
   3.2 Introduction of Concepts
   3.3 Types of Grounding Systems
   3.4 Bonding of Structural Elements
   3.5 General Comments: Floating Circuits and Test
       Verification
4. GROUNDING ARCHITECTURE REQUIREMENTS/SELECTION CRITERIA
   4.1 Size of Spacecraft
   4.2 Specific Implementations
       4.2.1 Main Power Distribution System: Single or
             Multiple Voltages
       4.2.2 Ground Fault Isolation of the Main Power Bus
       4.2.3 Power Sources
       4.2.4 Power User Load Isolation From Power
             Distribution System
       4.2.5 General Interface Circuits (Command, Signal,
             Data, etc.)
       4.2.6 Attitude Control Elements
       4.2.7 RF Interfaces
       4.2.8 Pyro Firing Unit
       4.2.9 Other Special Items, including Cable Overshields
   4.3 Interface Isolation Circuits
   4.4 Grounding of Support Equipment
   4.5 Heritage Spacecraft
FIGURES
TABLES
APPENDICES
A Sample Ground Trees For Large Complex Spacecraft

Defines describes spacecraft grounding architecture options at the system level. Implementation of good electrical grounding architecture is an important part of overall mission success for spacecraft.

DocumentType
Standard
PublisherName
National Aeronautics and Space Administration
Status
Current

BS ISO 14302:2002 Aerospace series. Space systems. Electromagnetic compatibility requirements
NASA STD 4005(INT) : 2006 LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD
ISO 14302:2002 Space systems Electromagnetic compatibility requirements

MIL-STD-1773 Base Document:1988 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
MIL-STD-1576 Base Document:1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS
MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

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