• NASA STD 5019(INT) : 2006

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE

    Available format(s): 

    Superseded date:  07-01-2008

    Language(s): 

    Published date:  01-01-2006

    Publisher:  National Aeronautics and Space Administration

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

    DOCUMENT HISTORY LOG
    FOREWORD
    1. SCOPE
       1.1 Introduction
       1.2 Purpose
       1.3 Applicability
       1.4 Responsibilities
    2. APPLICABLE DOCUMENTS
       2.1 General
       2.2 Government Documents
       2.3 Non-Government Documents
       2.4 Order of Precedence
    3. ACRONYMS AND DEFINITIONS
       3.1 Acronyms
       3.2 Definitions
    4. REQUIREMENTS
       4.1 Fracture Control Classification of Parts
           4.1.1 Non-Fracture-Critical Parts
           4.1.2 Fracture-Critical Parts
       4.2 Methodology for Assessing Fracture-Critical
           Hardware
           4.2.1 Damage Tolerant Analysis
           4.2.2 Damage Tolerant Testing
           4.2.3 Fleet Leader Testing
           4.2.4 General Damage Tolerance Requirements
       4.3 Tracking for Fracture-Critical Parts
           4.3.1 Materials
           4.3.2 Design, Analysis, and Hardware Configuration
           4.3.3 Load History
           4.3.4 Flaw Screening
       4.4 Fracture Control Documentation
           4.4.1 Fracture Control Plan
           4.4.2 Engineering Drawings
           4.4.3 Fracture Control Summary Report (FCSR)
           4.4.4 Presentation Summarizing the Fracture Control
                 Program
           4.4.5 Detailed Fracture Control Analysis Report
           4.4.6 Inspection Report
           4.4.7 Test Report
           4.4.8 Load/Use History
       4.5 Verification
       4.6 Alternatives
       4.7 Other Requirements
    5 GUIDANCE
       5.1 Reference Documents

    Abstract - (Show below) - (Hide below)

    Establishes the fracture control requirements for all human-rated spaceflight systems including payloads, propulsion systems, orbital support equipment, and planetary habitats.

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

    Development Note Expires 11 Sept 2007. (09/2006)
    Document Type Standard
    Publisher National Aeronautics and Space Administration
    Status Superseded
    Superseded By

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

    ASTM E 2981 : 2015 Standard Guide for Nondestructive Testing of the Composite Overwraps in Filament Wound Pressure Vessels Used in Aerospace Applications

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

    NASA STD 5017 : 2015 DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS
    NASA STD 5009(INT) : 2006 NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS
    NASA HDBK 5010 : 0 FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE
    API 579-1 : 2016 FITNESS-FOR-SERVICE
    MIL-HDBK-6870 Revision B:2012 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
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