NASA HDBK 6025 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS
16-08-2024
24-04-2014
DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS AND DEFINITIONS
4. GENERAL
5. NONCONFORMING TI ALLOYS
6. MITIGATING THE PROCUREMENT OF NONCONFORMING TI ALLOYS
APPENDICES
A - Reference Documents and Military Specifications
B - Chronological History for Nonconforming Ti Alloy GIDEPs
C - Screening of Ti Alloy Parts for In-Process Projects at JPL
D - Example Suspect Material Certifications
E - Example of an Acceptable ('Clean') Certification Package
F - Raw Material Supplier Audit Checklist
G - Example Quality Clause Entitled 'Raw Material Traceability'
H - Mechanical Test Results in Material Certification versus
In-House Test Data for Ti-6Al-4V
Specifies guideline procedures and processes that will help mitigate the procurement of nonconforming wrought titanium (Ti) alloys for National Aeronautics and Space Administration (NASA) flight applications.
| DocumentType |
Handbook
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Superseded
|
| SupersededBy |
| SAE AMS 6910 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 8AL - 1MO - 1V, DUPLEX ANNEALED |
| SAE AMS 6925 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED |
| SAE AMS T 9047 : 2003 | TITANIUM AND TITANIUM ALLOY, BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY |
| SAE AMS 6900 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 5AL - 2.5SN, ANNEALED |
| ASTM B 348 : 2013 : REDLINE | Standard Specification for Titanium and Titanium Alloy Bars and Billets |
| SAE AMS 4915 : 2013 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
| SAE AMS 6932 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AMS 4989 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 2.5V, ANNEALED |
| SAE AMS 4918 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 6921 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED AND AGED |
| SAE AMS T 9046 : 2002 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP, AND PLATE |
| SAE AMS4990C | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4919 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 6AL - 2SN - 4ZR - 2MO - 0.08SI DUPLEX ANNEALED |
| SAE AMS 6905 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 2.0MO, DUPLEX ANNEALED |
| SAE AMS 6940 : 2011 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3.0AL - 2.5V, ANNEALED |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE |
| SAE AMS 6907 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, DUPLEX ANNEALED |
| SAE AMS 6915 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 7.0AL - 4.0MO, ANNEALED |
| SAE AMS 4917 : 2012 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
| SAE AMS 6931 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, ANNEALED |
| MMPDS 06 : 2011 | METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) - COMPLETE SET INCLUDES 9 CHAPTERS |
| SAE AS 9100D : 2016 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 2750 : 2012 | PYROMETRY |
| SAE AMS 4958 : 2013 | TITANIUM ALLOY BARS AND RODS, 3AL - 8V - 6CR - 4MO - 4ZR, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND CENTERLESS GROUND OR PEELED AND POLISHED |
| SAE AMS 6926 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 6920 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
| SAE ARP 1917 : 2002 | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE AMS 4910 : 2017 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED |
| SAE AMS 4907 : 2013 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6.0AL - 4.0V, EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 4926 : 2015 | TITANIUM ALLOY, BARS, WIRE, AND RINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| SAE AMS4957F | TITANIUM ALLOY, ROUND BAR AND WIRE, 3AI - 8V - 6CR - 4MO - 4ZR, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND COLD DRAWN |
| SAE AMS 4945 : 2014 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
| SAE AMS 4988 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED |
| SAE AMS H 81200 : 2014 | HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
| SAE AMS 4979 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4978 : 2014 | TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 4904 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4909 : 2016 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
| SAE AMS6906B | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION HEAT TREATED AND AGED |
| NASA HDBK 8739.18 : 2008 | PROCEDURAL HANDBOOK FOR NASA PROGRAM AND PROJECT MANAGEMENT OF PROBLEMS, NONCONFORMANCES, AND ANOMALIES - MEASUREMENT SYSTEM IDENTIFICATION: METRIC |
| SAE AMS 4903 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED |
| SAE AMS 6930 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4916 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
| SAE AMS 4944 : 2015 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED |
| SAE AMS 6936 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 6935 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 6.0V - 2.0SN, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AMS 6901 : 2015 | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
| SAE AMS 4928 : 2016 | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
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