NASA MSFC STD 557 : 2012
Current
The latest, up-to-date edition.
THREADED FASTENERS, TITANIUM ALLOYS, USAGE CRITERIA FOR LAUNCH VEHICLES AND SPACECRAFT APPLICATIONS
Hardcopy , PDF
English
15-02-2012
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
|
| Pages |
9
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Current
|
| Supersedes |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| SAE AMS5525J | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Heat Treated |
| MIL-I-45914 Revision A:1991 | Insert, Screw Thread - Locked in, Key Locked, General Specification for |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| MIL I 45932 : 0 | INSERT, SCREW THREAD, THIN WALL, LOCK IN |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| MIL-PRF-46010 Revision H:2013 | Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting NATO Code - S-1738 |
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