SAE AMS2774E
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS
Hardcopy , PDF
29-05-2020
English
01-01-2016
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Superseded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 AMS5225F | IRON-NICKEL ALLOY, STRIP, 49FE - 5.3CR - 42NI - 2.5TI - 0.55AL, SOLUTION HEAT TREATED, COLD ROLLED, 50% REDUCTION |
SAE AMS5663N | 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 MA3378C | BOLTS AND SCREWS, UNS N07001, TENSILE STRENGTH 1210 MPA, THREAD AND FILLET RADIUS ROLLED BEFORE AGING, PROCUREMENT SPECIFICATION, METRIC |
SAE AMS5532G | 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 AMS5894D | COBALT ALLOYS, BARS, SHEET, AND PLATE, 60CO - 28CR - 4.5W - 1.15C, SOLUTION HEAT TREATED |
SAE AMS5882D | 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 AMS5662N | 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 AMS5886C | 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 AMS5699G | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WIRE, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, SPRING TEMPER, PRECIPITATION HARDENABLE |
SAE AMS5707M | 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 AMS5873F | 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 AMS5581F | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED TUBING, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), ANNEALED |
SAE AMS5704K | 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 AMS5582F | 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 AMS5608G | 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 AS7467B | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, STRESS RUPTURE RATED, PROCUREMENT SPECIFICATION |
SAE AMS5599H | 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 AMS5709H | 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 AMS5667N | 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 AMS5715F | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60.5NI - 23CR - 14FE - 1.4AL, ANNEALED |
SAE AMS5842G | 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 AMS5711E | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 65NI - 15.8CR - 15.2MO - 0.30AL - 0.05LA, SOLUTION HEAT TREATED |
SAE AMS5712K | 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 AMS5889C | 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 AMS5759M | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGING STOCK, FORGINGS, AND RINGS 52CO - 20CR - 10NI - 15W |
SAE AMS5536N | 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 AMS5553G | NICKEL, SHEET AND STRIP, LOW (0.02 MAX) CARBON, ANNEALED |
SAE AMS5542N | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED |
SAE AMS5586G | 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 AMS5544K | 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 AMS5605F | 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 AMS5870E | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 60.5NI - 23CR - 14FE - 0.35TI - 1.4AL, SOLUTION HEAT TREATED |
SAE AMS5537H | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL, AND PLATE, 52CO - 20CR - 10NI - 15W, SOLUTION HEAT TREATED |
SAE AMS5221E | 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 AMS5888C | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, PLATE, 54NI - 22CR - 12.5CO - 9.0MO - 1.2AL, ANNEALED |
SAE AMS5541G | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET AND STRIP 73NI - 15.5CR - 2.4TI - 0.7AL - 7.0FE ANNEALED |
SAE AMS5702D | 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 AMS5540N | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 74NI - 15.5CR - 8.0FE, ANNEALED |
SAE AS7466E | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, FATIGUE RATED, PROCUREMENT SPECIFICATION |
SAE AMS5607E | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 73NI - 7.0CR - 16.5MO, SOLUTION HEAT TREATED |
SAE AS7468B | BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30035, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
SAE AMS2750E | PYROMETRY |
SAE AMS5583E | 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 AMS5769F | 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 AMS5598E | 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 AMS5664F | 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 AMS5660L | 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 AMS5714D | ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT-RESISTANT, 73NI - 15.5CR - 2.5TI - 0.70AL - 7.0FE, PRECIPITATION-HARDENABLE |
SAE AMS5891B | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60NI - 22CR - 2.0MO - 14W - 0.35AL - 0.03LA, ANNEALED |
SAE AMS5772E | 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 AMS5884D | 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 AMS5874C | 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 AMS5545F | 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 ARP1820B | CHORD METHOD OF EVALUATING SURFACE MICROSTRUCTURAL CHARACTERISTICS |
SAE AMS5670F | 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 AMS5597G | 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 AS7237 | 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 AS7475D | BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30159, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
SAE AMS5871F | ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 21CR - 32.5NI - 0.38TI - 0.38AL - 45FE, SOLUTION HEAT TREATED |
SAE AMS5589F | 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 AMS5887D | 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 AMS2769B | HEAT TREATMENT OF PARTS IN A VACUUM |
SAE AS7471G | 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 AMS5668J | 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 AMS5698G | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WIRE, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, NO. 1 TEMPER, PRECIPITATION HARDENABLE |
SAE AMS5747D | 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 AMS5844H | ALLOY, CORROSION-RESISTANT, ROUND BARS, 20CR - 35NI - 35CO - 10MO, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED, SOLUTION HEAT TREATED AND WORK STRENGTHENED |
SAE AMS5771F | 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 AMS5706M | 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 AMS5671G | 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 AMS5701E | 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 AMS5588G | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WELDED TUBING, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
SAE AMS5596L | 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 AMS5833D | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, ROUND WIRE 20CR - 15NI - 40CO - 7.0MO - 16FE SOLUTION HEAT TREATED AND COLD DRAWN |
SAE AMS5893B | 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 AMS5590F | 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 AMS5223F | IRON-NICKEL ALLOY, STRIP, 49Fe 5.3Cr 42Ni 2.5Ti 0.55Al, SOLUTION HEAT TREATED, COLD ROLLED, 10% REDUCTION |
SAE AMS5585H | ALLOY, CORROSION AND HEAT RESISTANT, WELDED TUBING, 32FE - 21CR - 20NI - 20CO - 3MO - 2.5W - 1.0CB (NB) - 0.15N, SOLUTION HEAT TREATED |
SAE AMS5708L | 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 AMS5872E | 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 AMS5666H | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, EXTRUSIONS, AND RINGS, 62NI - 21.5CR - 9.0MO - 3.65CB (NB), ANNEALED |
SAE AMS5665N | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS, 74NI - 15.5CR - 8.0FE |
SAE AMS5550F | ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT, 80NI - 15.5CR - 0.62TI - 3.25AL, ANNEALED |
SAE AMS5766E | ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 21CR - 32.5NI - 0.38TI - 0.38AL - 45FE, SOLUTION HEAT TREATED |
SAE AMS5661F | 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 AMS5876D | 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 AMS5892B | 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 AMS5587F | 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 AMS5580L | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING 74NI - 15.5CR - 8.0FE, ANNEALED |
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