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NASA STD 5019(INT) : 2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

Superseded date

01-07-2008

Published date

01-01-2006

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

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

DevelopmentNote
Expires 11 Sept 2007. (09/2006)
DocumentType
Standard
PublisherName
National Aeronautics and Space Administration
Status
Superseded
SupersededBy

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

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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