SAE AMS 2774 : 2016
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS
Available format(s)
Hardcopy , PDF
Superseded date
29-05-2020
Superseded by
Language(s)
English
Published date
01-01-2016
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
APPENDIX A
Describes the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts made of wrought nickel or cobalt alloys, of raw materials during fabrication, and of fabricated assemblies in which wrought nickel or cobalt alloys are the primary structural components.
| Committee |
AMS-F
|
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| ASTM F 3301 : 2018 | Standard for Additive Manufacturing – Post Processing Methods – Standard Specification for Thermal Post-Processing Metal Parts Made Via Powder Bed Fusion |
| ASTM F 3056 : 2014 | Standard Specification for Additive Manufacturing Nickel Alloy (UNS N06625) with Powder Bed Fusion |
| ASTM F 3213 : 2017 | Standard for Additive Manufacturing – Finished Part Properties – Standard Specification for Cobalt-28 Chromium-6 Molybdenum via Powder Bed Fusion |
| ASTM F 3056 : 2014 : EDT 1 | Standard Specification for Additive Manufacturing Nickel Alloy (UNS N06625) with Powder Bed Fusion |
| ASTM F 3055 : 2014 | Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion |
| ASTM F 3055 : 2014 : EDT 1 | Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion |
| SAE AMS 7000 : 2018 | LASER-POWDER BED FUSION (L-PBF) PRODUCED PARTS, NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, 62NI - 21.5CR - 9.0MO - 3.65NB STRESS RELIEVED, HOT ISOSTATIC PRESSED AND SOLUTION ANNEALED |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| NASA PRC 2003 : 2011 | PROCESS SPECIFICATION FOR THE HEAT TREATMENT OF NICKEL ALLOYS |
| SAE AMS 5917 : 2011 | METAL INJECTION MOLDED NICKEL BASED, ALLOY 718 PARTS, HOT ISOSTATICALLY PRESSED, SOLUTIONED AND AGED |
| NASA MSFC SPEC 3717 : 2017 | SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
| SAE AMS 5225 : 2014 | IRON-NICKEL ALLOY, STRIP, 49FE - 5.3CR - 42NI - 2.5TI - 0.55AL, SOLUTION HEAT TREATED, COLD ROLLED, 50% REDUCTION |
| SAE AMS 5663 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE MA 3378 : 2012 | BOLTS AND SCREWS, UNS N07001, TENSILE STRENGTH 1210 MPA, THREAD AND FILLET RADIUS ROLLED BEFORE AGING, PROCUREMENT SPECIFICATION, METRIC |
| SAE AMS 5532 : 2012 | IRON ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 30FE - 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0CB(NB) - 0.15N, SOLUTION HEAT TREATED |
| SAE AMS 5877 : 2012 | IRON ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 29FE - 22CR - 21NI - 18.5CO - 3.2MO - 2.8W - 0.78TA - 0.30AL - 0.05LA - 0.20N, SOLUTION HEAT TREATED |
| SAE AMS 5894 : 2016 | COBALT ALLOYS, BARS, SHEET, AND PLATE, 60CO - 28CR - 4.5W - 1.15C, SOLUTION HEAT TREATED |
| SAE AMS 5882 : 1989 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, FORGINGS 55NI 15CR 17CO 5.0MO 3.5TI 4.0AI 0.025B, SOLUTION, STABILIZATION AND PRECIPITATION HEAT TREATED, POWDER-METALLURGY PRODUCT |
| SAE AS 7236 : 2012 | RIVETS, ALLOY, CORROSION AND HEAT RESISTANT 52CO-20CR-10NI-15W SOLUTION HEAT TREATED PROCUREMENT SPECIFICATION FOR |
| BB-H-1168 Revision D:2010 | HELIUM, TECHNICAL |
| SAE AMS 5755 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 64NI - 5.0CR - 24.5MO - 5.5FE, SOLUTION HEAT TREATED |
| SAE AMS 5662 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AI - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
| SAE AMS 5886 : 2014 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 50NI - 20CR - 20CO - 5.8MO - 2.2TI - 0.45AL CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 2100 DEGREES F (1149 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5699 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WIRE, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, SPRING TEMPER, PRECIPITATION HARDENABLE |
| SAE AMS 5707 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED 1825 TO 1900 DEGREES F (996 TO 1038 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5873 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 65NI - 15.8CR - 15.2MO - 0.30AI - 0.05LA, CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED |
| MIL-PRF-27407 Revision D:2014 | PROPELLANT PRESSURIZING AGENT, HELIUM |
| SAE AMS 5581 : 2010 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED TUBING, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), ANNEALED |
| SAE AMS 5704 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, FORGINGS 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1825 TO 1900 DEGREES F (996 TO 1038 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5582 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE TO 155 KSI (1069 MPA) TENSILE STRENGTH |
| SAE AMS 5608 : 2016 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
| SAE AS 7232 : 2012 | RIVETS, SOLID AND TUBULAR, NICKEL ALLOY CORROSION AND HEAT RESISTANT 74NI - 15.5CR - 8.0FE PROCUREMENT SPECIFICATION FOR |
| CGA G 11.1 : 2016 | COMMODITY SPECIFICATION FOR ARGON |
| SAE AS 7467 : 2013 | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, STRESS RUPTURE RATED, PROCUREMENT SPECIFICATION |
| SAE AMS 5599 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED |
| SAE AMS 4676 : 2017 | NICKEL-COPPER ALLOY, CORROSION-RESISTANT, BARS AND FORGINGS, 66.5NI - 3.0AL - 0.62TI - 28CU, HOT-FINISHED, PRECIPITATION HARDENABLE |
| SAE AMS 5709 : 2013 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS AND FORGINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREE F (1079 DEGREE C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| MIL A 18455 : C | ARGON, TECHNICAL |
| SAE AMS 5667 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE EQUALIZED, PRECIPITATION HARDENABLE |
| SAE AMS 5715 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60.5NI - 23CR - 14FE - 1.4AL, ANNEALED |
| SAE AMS 5842 : 2016 | COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED AND WORK STRENGTHENED |
| SAE AMS 5711 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 65NI - 15.8CR - 15.2MO - 0.30AL - 0.05LA, SOLUTION HEAT TREATED |
| SAE AMS 5712 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 53NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| ASTM E 384 : 2017 : REDLINE | Standard Test Method for Microindentation Hardness of Materials |
| SAE AMS 5889 : 2015 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET AND STRIP, 54NI - 22CR - 12.5CO - 9.0MO - 1.2AL, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED |
| SAE AMS 5759M : 2015 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGING STOCK, FORGINGS, AND RINGS 52CO - 20CR - 10NI - 15W |
| SAE AMS 5536 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
| SAE AMS 5553 : 2012 | NICKEL, SHEET AND STRIP, LOW (0.02 MAX) CARBON, ANNEALED |
| SAE AMS 5542 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED |
| SAE AMS 5586 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WELDED TUBING, 57NI - 19.5CR - 13.5CO - 4.2MO - 2.9TI - 1.4AL - 0.006B - 0.08ZR, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, ANNEALED |
| SAE AMS 5544 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED |
| SAE AMS 5605 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 41.5NI - 16CR - 37FE - 2.9CB(NB) - 1.8TI, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5870 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 60.5NI - 23CR - 14FE - 0.35TI - 1.4AL, SOLUTION HEAT TREATED |
| SAE AMS 5537 : 2012 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL, AND PLATE, 52CO - 20CR - 10NI - 15W, SOLUTION HEAT TREATED |
| SAE AMS 5221 E: 2012 | IRON-NICKEL ALLOY STRIP 49FE - 5.3CR - 42NI - 2.5TI - 0.55AL SOLUTION HEAT TREATED |
| SAE AS 7469 : 2011 | BOLTS AND SCREWS, UNS N07041 NICKEL ALLOY, CORROSION AND HEAT RESISTANT, 155 KSI, PROCUREMENT SPECIFICATION |
| ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
| SAE AMS 5888C : 2009(R2015) | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, PLATE, 54NI - 22CR - 12.5CO - 9.0MO - 1.2AL, ANNEALED |
| SAE AMS 5541 : 2013 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET AND STRIP 73NI - 15.5CR - 2.4TI - 0.7AL - 7.0FE ANNEALED |
| SAE AMS 5702 : 2007 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 41.5NI - 16CR - 37FE - 2.9CB (NB) - 1.8TI, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1750 DEGREES F (954 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5878 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 59NI - 22CR - 2MO - 14W - 0.35AI - 0.03LA, SOLUTION HEAT TREATED |
| SAE AMS 5540 : 2011 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 74NI - 15.5CR - 8.0FE, ANNEALED |
| SAE AS 7466 : 2014 | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, FATIGUE RATED, PROCUREMENT SPECIFICATION |
| SAE AMS 5607 E: 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 73NI - 7.0CR - 16.5MO, SOLUTION HEAT TREATED |
| SAE AS 7468 : 2012 | BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30035, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
| SAE AMS 2750 : 2012 | PYROMETRY |
| SAE AMS 5583 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, VACUUM MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE TO 170 KSI (1172 MPA) TENSILE STRENGTH |
| SAE AS 7246 : 2012 | INSERTS, SCREW THREADS, HELICAL COIL 72NI-15.5CR-0.95(CB+TA)-2.5TI-0.70AL-7.0FE CORROSION AND HEAT RESISTANT ALLOY PROCUREMENT SPECIFICATION FOR |
| SAE AMS 5769 : 2014 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0(CB+TA) - 0.15N - 32FE SOLUTION HEAT TREATED |
| SAE AMS 5598 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95 (CB (NB) + TA) - 2.5TI - 0.70AL - 7.0FE, CONSUMABLE ELECTRODE, REMELTED OR VACUUM INDUCTION MELTED, SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
| SAE AMS 5664 : 2017 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1950 DEGREES F (1066 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5660 : 2015 | NICKEL-IRON ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 12.5CR - 42.5NI - 6.0MO - 2.7TI - 0.015B - 34FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5714 : 2012 | ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT-RESISTANT, 73NI - 15.5CR - 2.5TI - 0.70AL - 7.0FE, PRECIPITATION-HARDENABLE |
| SAE AMS 5891 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60NI - 22CR - 2.0MO - 14W - 0.35AL - 0.03LA, ANNEALED |
| SAE AMS 5772 E: 2016 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
| SAE AS 7253 : 2015 | NUTS, SELF-LOCKING, NICKEL ALLOY, UNS N07001 CLASSIFICATION: 180 KSI/1400 DEGREES F, PROCUREMENT SPECIFICATION |
| SAE AMS 5884 : 2016 | IRON-NICKEL ALLOY, BARS, FORGINGS, AND RINGS, 42FE - 37.5NI - 14CO - 4.8CB(NB) - 1.6TI, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE MULTIPLE MELTED, HIGH TEMPERATURE, LOW EXPANSION |
| SAE AMS 5874 : 2012 | ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 29FE - 22CR - 21NI - 18.5CO - 3.2MO - 2.8W - 0.78TA - 0.30AL - 0.05ZR - 0.05LA - 0.20N SOLUTION HEAT TREATED |
| SAE AMS 5545 : 2010 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 54NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.5AL - 0.006B, VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATABLE, PRECIPITATION HEAT TREATED |
| SAE ARP 1820 : 2012 | CHORD METHOD OF EVALUATING SURFACE MICROSTRUCTURAL CHARACTERISTICS |
| SAE AMS 5670 : 2012 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS - 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5597 : 2016 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1950 DEGREES F (1066 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5606 : 2013 | ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE 41.5NI - 16CR - 37FE - 2.9CB (NB) - 1.8TI CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1750 DEGREES F (954 DEGREES C) SOLUTION HEAT TREATED |
| SAE AS 7237 : 2012 | RIVETS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT 47.5NI-22CR-1.5CO-9.0MO-0.60W-18.5FE SOLUTION HEAT TREATED PROCUREMENT SPECIFICATION FOR |
| SAE AS 7475 : 2015 | BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30159, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
| SAE AMS 5871 : 2015 | ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 21CR - 32.5NI - 0.38TI - 0.38AL - 45FE, SOLUTION HEAT TREATED |
| SAE AMS 5589 : 2013 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SEAMLESS TUBING 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C), SOLUTION HEAT TREATED |
| SAE AMS 5887 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 54NI - 22CR - 12.5CO - 9.0MO - 1.2AL, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED |
| MIL-PRF-27201 Revision E:2013 | PROPELLANT, HYDROGEN |
| SAE AMS 2769 : 2014 | HEAT TREATMENT OF PARTS IN A VACUUM |
| SAE AS 7471 : 2015 | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07001 TENSILE STRENGTH 165 KSI, CORROSION AND HEAT RESISTANT, PROCUREMENT SPECIFICATION |
| MIL-PRF-27401 Revision G:2013 | Propellant Pressurizing Agent, Nitrogen |
| SAE AMS 5668 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 72NI - 15.5CR - 7.0FE - 2.5TI - 1.0CB (NB) - 0.70AL, 2100 DEGREES F (1149 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5698 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WIRE, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, NO. 1 TEMPER, PRECIPITATION HARDENABLE |
| SAE AMS 5747 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5844 : 2014 | ALLOY, CORROSION-RESISTANT, ROUND BARS, 20CR - 35NI - 35CO - 10MO, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED, SOLUTION HEAT TREATED AND WORK STRENGTHENED |
| SAE AMS 5771 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 74NI - 7.0CR - 16.5 MO, SOLUTION HEAT TREATED |
| SAE AMS 5846 : 2016 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 53NI - 15CR - 18.5CO - 5.0MO - 3.2TI - 4.2AL - 0.03B, DOUBLE VACUUM MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5706 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.006B - 0.05ZR, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1825 TO 1900 DEGREES F SOLUTION HEAT TREATED |
| SAE AMS 5671 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5701 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 41.5NI - 16CR - 37FE - 2.9CB (NB) - 1.8TI, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5754 : 2007 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
| SAE AMS 5746 : 2012 | ALLOY, CORROSION AND HEAT RESISTANT, BARS AND FORGINGS - 15CR - 45NI - 4.1MO - 4.1W - 3.0TI - 1.0AL - 31FE (D979) CONSUMABLE ELECTRODE VACUUM MELTED, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5588G : 2010 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WELDED TUBING, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
| SAE AMS 5596 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED |
| CGA G 10.1 : 2016 | COMMODITY SPECIFICATION FOR NITROGEN |
| SAE AMS 5833 : 2014 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, ROUND WIRE 20CR - 15NI - 40CO - 7.0MO - 16FE SOLUTION HEAT TREATED AND COLD DRAWN |
| SAE AMS 5893 : 2012 | IRON-NICKEL ALLOY, BARS, FORGINGS, AND RINGS, 42FE - 37.5NI - 14CO - 4.8(CB + TA)(NB + TA) - 1.6TI, SOLUTION HEAT TREATED, SHORT-TIME PRECIPITATION HARDENABLE MULTIPLE MELTED, HIGH TEMPERATURE, LOW EXPANSION |
| SAE AMS 5590 : 2010 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SEAMLESS TUBING, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1950 DEGREE F (1066 DEGREE C) SOLUTION HEAT TREATED |
| SAE AMS 5223 : 2012 | IRON-NICKEL ALLOY, STRIP, 49Fe 5.3Cr 42Ni 2.5Ti 0.55Al, SOLUTION HEAT TREATED, COLD ROLLED, 10% REDUCTION |
| SAE AMS 5585 : 2016 | ALLOY, CORROSION AND HEAT RESISTANT, WELDED TUBING, 32FE - 21CR - 20NI - 20CO - 3MO - 2.5W - 1.0CB (NB) - 0.15N, SOLUTION HEAT TREATED |
| SAE AMS 5708 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, WIRE FORGINGS, AND RINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREES F (1079 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 5872 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 48NI - 20CR - 20CO - 5.9MO - 2.2TI - 0.45AL, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, SOLUTION HEAT TREATED |
| SAE AMS 5666H : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, EXTRUSIONS, AND RINGS, 62NI - 21.5CR - 9.0MO - 3.65CB (NB), ANNEALED |
| SAE AMS 5665 : 2012 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS, 74NI - 15.5CR - 8.0FE |
| SAE AMS 5550F :1988(S2017) | ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT, 80NI - 15.5CR - 0.62TI - 3.25AL, ANNEALED |
| SAE AMS5766E:2014 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 21CR - 32.5NI - 0.38TI - 0.38AL - 45FE, SOLUTION HEAT TREATED |
| SAE AMS 5661 : 2012 | NICKEL-IRON ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS - 42.5NI - 12.5CR - 5.8MO - 2.9TI - 0.015B - 35FE - CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5876 : 2014 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, STRIP, 20CR - 15NI - 40CO - 7.0MO - 16FE, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED AND COLD ROLLED |
| SAE AMS 5892 : 2014 | ALLOY, SHEET AND STRIP, 42FE - 37.5NI - 14CO - 4.8CB (NB) - 1.6TI, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE, MULTIPLE MELTED, HIGH TEMPERATURE, LOW EXPANSION |
| ASTM E 8/E8M : 2016-09 | TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS |
| SAE AMS 5587 : 2016 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SEAMLESS TUBING, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
| SAE ARP 1962 : 1995 | TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL |
| SAE AMS 5580 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING 74NI - 15.5CR - 8.0FE, ANNEALED |
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