NASA STD 5007 : 2001
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GENERAL FRACTURE CONTROL REQUIREMENTS FOR MANNED SPACEFLIGHT SYSTEMS
07-01-2019
12-01-2013
FOREWORD
1. INTRODUCTION
1.1 Scope
1.2 Fracture Control Authority
1.3 Alternate Requirements
1.4 Other Requirements
1.5 Prerogatives of the Government
2. FRACTURE CONTROL IMPLEMENTATION
2.1 Fracture Control Applicability
2.2 Program Specific Fracture Control Requirements
2.3 Selection Process
2.4 Fracture Control Documentation
2.4.1 Fracture Control Plan
2.4.2 Fracture Control Summary Report
2.4.3 Supporting Data
3. DAMAGE TOLERANCE REQUIREMENTS
3.1 Load Spectrum Requirements
3.2 Analysis Requirements
3.3 Test Requirements
4. SPECIAL PROCESSING FOR FRACTURE CRITICAL PARTS
4.1 Traceability
4.2 Non-destructive evaluation (NDE)
4.3 Detected Cracks
Describes the fracture control requirements for all manned spaceflight systems and all payloads on manned spaceflight systems.
DocumentType |
Standard
|
PublisherName |
National Aeronautics and Space Administration
|
Status |
Superseded
|
SupersededBy |
NASA SP 3421 : 2011 | PROBABILISTIC RISK ASSESSMENT PROCEDURES GUIDE FOR NASA MANAGERS AND PRACTITIONERS |
NASA MSFC RQMT 3479 : 2006 | FRACTURE CONTROL REQUIREMENTS FOR COMPOSITE AND BONDED VEHICLE AND PAYLOAD STRUCTURES |
NASA STD 5009(INT) : 2006 | NONDESTRUCTIVE EVALUATION REQUIREMENTS FOR FRACTURE CRITICAL METALLIC COMPONENTS |
NASA MSFC HDBK 505 : 2005 | STRUCTURAL STRENGTH PROGRAM REQUIREMENTS |
NASA HDBK 5010 : 0 | FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE |
NASA JSC 25863 : 2009 | FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE |
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.