NASA STD 5018 : 2011
Current
The latest, up-to-date edition.
STRENGTH DESIGN AND VERIFICATION CRITERIA FOR GLASS, CERAMICS, AND WINDOWS IN HUMAN SPACE FLIGHT APPLICATIONS
Hardcopy , PDF
English
27-11-2017
DOCUMENT HISTORY LOG
FOREWORD
LIST OF EQUATIONS
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. REQUIREMENTS
5. VERIFICATIONS
APPENDICES
A - Data Item Descriptions
B - Reference Documents
The purpose of this Standard is to specify the minimum structural design requirements for the design, development, and verification of windows, glass, and ceramic structure included in National Aeronautics and Space Administration (NASA) vehicles/elements, habitats, space suits, all orbital support equipment (OSE), and flight support equipment (FSE).
DocumentType |
Standard
|
Pages |
48
|
PublisherName |
National Aeronautics and Space Administration
|
Status |
Current
|
NASA STD 5001 : 2014 | STRUCTURAL DESIGN AND TEST FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
NASA JSC 65828 : 2011 | STRUCTURAL DESIGN REQUIREMENTS AND FACTORS OF SAFETY FOR SPACEFLIGHT HARDWARE |
NASA STD 5019 : 2016 | FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE |
NASA JSC 08080-2 : 2015 | JSC DESIGN AND PROCEDURAL STANDARDS |
NASA HDBK 6007 : 2013 | HANDBOOK FOR RECOMMENDED MATERIAL REMOVAL PROCESSES FOR ADVANCED CERAMIC TEST SPECIMENS AND COMPONENTS |
NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
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