THREADED FASTENERS, TITANIUM ALLOYS, USAGE CRITERIA FOR LAUNCH VEHICLES AND SPACECRAFT APPLICATIONS

Published date

01-01-2012

Publisher

National Aeronautics and Space Administration

DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. NOTES

Sets up criteria for use of titanium alloy threaded fastener systems for launch vehicles, spacecraft, and associated equipment.

DocumentType	Standard
PublisherName	National Aeronautics and Space Administration
Status	Current

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