![header thumbnail](/images/publishers\nasa_cover.gif)
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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
![header thumbnail](/images/publishers\nasa_cover.gif)
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
07-01-2008
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
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.