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
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5525 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED |
| NAS 4004 : 2004 | FASTENER, 6AL-4V TITANIUM ALLOY, EXTERNALLY THREADED, 160 KSI FTU, 95 KSI FSU, 450 DEGREES F |
| SAE AMS 5758 : 2014 | ALLOY, CORROSION-RESISTANT, BARS, 20CR - 35NI - 35CO - 10MO, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED, SOLUTION HEAT TREATED FOR WORK STRENGTHENING |
| MIL-I-45914 Revision A:1991 | INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| NASM8846:2011 | INSERT, SCREW-THREAD, HELICAL COIL |
| SAE AMS 5732 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| NAS621:2013 | FASTENERS, TITANIUM ALLOY PROCUREMENT SPECIFICATION |
| 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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