Browse Topic: Heat resistant materials

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Steel Tubing, Seam-Free, Round, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), 95.0 ksi (655 MPa) Tensile StrengthAMS6374F (Current)11/25/2025
This specification covers an aircraft-quality, low-alloy steel in the form of round, non-welded tubing free from OD surface seams.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welded Tubing, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)AMS6373K (Current)11/25/2025
This specification covers an aircraft-quality, low-alloy steel in the form of welded tubing.
AMS E Carbon and Low Alloy Steels Committee
Cobalt Alloy, Corrosion and Heat Resistant, Hardfacing Rod and Wire, 62Co - 27 Cr - 2.9Ni - 5.5MoAMS5819B (Current)11/25/2025
This specification covers a corrosion and heat-resistant cobalt alloy in the form of welding rods or wrought wire.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant, Flat Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Treated, Cold Drawn or Cold Rolled and Aged, Consumable Electrode Remelted AMS5810C (Current)11/25/2025
This specification covers a corrosion and heat resistant steel in the form of flat wire.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Bars and Forgings 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Consumable Electrode Remelted Solution Heat Treated, Sub-Zero Cooled, Equalized, and Over-Tempered AMS5743L (Current)11/25/2025
This specification covers a corrosion and heat-resistant steel in the form of bars, forgings, and forging stock. These products have been used typically for parts requiring oxidation resistance and high strength up to 800 °F (427 °C) and where such parts may require welding during fabrication, but usage is not limited to such applications.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Sheet, Strip and Plate, 18Cr - 13Ni - 2.5Mo (SAE 30316), Solution Heat TreatedAMS5524N (Current)11/25/2025
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness (see 8.7).
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate, 13Cr - 2.0Ni - 3.0W, AnnealedAMS5508H (Current)11/25/2025
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat Resistant, Investment Castings, 65Ni - 28Mo - 5.5Fe - 0.4V (N-12MV), As-CastAMS5396G (Current)11/25/2025
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat Resistant, Investment Castings 73ni - 12cr - 4.5mo - 2.0cb - 0.70ti - 0.05c - 6.0al - 0.010b - 0.10zr, Vacuum Cast, As-CastAMS5377H (Current)11/25/2025
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion Heat Resistant Alloys Committee
Manufacturing of Thermoplastic Composite Parts with Press Forming TechnologyF-0080-2024-13625/7/2024
Thermoplastic composites are serious competitor for classic epoxy composites. They have comparable properties to epoxy composites, but characterize much lower processing costs. There are several methods of manufacturing the components from thermoplastic composites. One of the most interesting method in terms of efficiency is thermoforming on a press. This technology allows to product of the aircraft parts such as: ribs, brackets, covers, stiffeners. Thermoplastic composites are resistant to most solvents such as grease, oil and aviation fuel. They are also non-flammable and heat-resistant. This all makes them suitable for use in aircraft as upholstery, casing or elements around the tank. PZL Mielec has been developing press thermoforming technologies since 2016 and is the owner of the several patents in this area.
Głodzik, Marcin, Wojtuszewski, Radosław, Farbaniec, Konrad, Sienicki, Jarosław, Banaś, Aleksander, Gałaczyński, Tomasz
Elastomer: Nitrile Rubber (NBR) Synthetic Oil Resistant Sheets, 65 to 75 Type A Hardness for Products in Engine Oil SystemsAMS3786 (Current)10/22/2021
This specification covers a nitrile rubber (NBR) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7289 specification.
AMS CE Elastomers Committee
Adhesion Promoter for Polysulfide Sealing CompoundsAMS3100E (Current)10/19/2021
This specification covers adhesion promoters in liquid form for use with aerospace sealing compounds.
AMS G9 Aerospace Sealing Committee
Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 72Ni - 15.5Cr - 1.0Cb(Nb) - 2.4Ti - 0.70Al - 7.0FeAMS5778K (Current)10/18/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion Heat Resistant Alloys Committee
Insulating Component, Molded, Electrical, Heat Shrinkable, Connector and Cable Accessory, Sealing Strain Relief, General Specification ForAS5258A (Current)10/13/2021
This specification covers connector and cable accessory heat shrinkable, electrical insulating, molded components fabricated from various polymer based compositions. These components are intended for use as connector and cable accessory components to provide strain relief, electrical insulation, and environmental sealing.
AE-8C1 Connectors Committee
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 45.5Ni - 25.5Cr - 3.2Co - 3.2Mo - 3.2W - 18.5Fe Solution Heat TreatedAMS5593H (Current)9/21/2021
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Bolts and Screws, Steel, UNS S66286 Tensile Strength 160 ksi, Procurement SpecificationAS4506C (Current)9/1/2021
This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
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 TreatedAMS5525L (Current)9/1/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate 0.0010 inch (0.025 mm) and above in nominal thickness (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll ThreadedAS7479E (Current)8/27/2021
This specification covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
E-25 General Standards for Aerospace and Propulsion Systems
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Foil 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) Cold Rolled and AnnealedAMS5879E (Current)8/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Sheet, Strip, Foil, and Plate 15Cr - 7.1Ni - 2.5Mo - 1.1Al Solution Heat Treated, Precipitation HardenableAMS5520H (Current)7/23/2021
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, foil, and plate 0.0015 inch (0.038 mm) and greater in nominal thickness.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Solution Heat TreatedAMS5513K (Historical)7/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Sealing Compound, Topcoat, Fuel Tank, Buna-N TypeAMSS4383C (Current)6/29/2021
This specification covers one type of one-component, air-drying protective coating which cures at room temperature.
AMS G9 Aerospace Sealing Committee
Iron-Nickel Alloy, Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat Treated, Cold Rolled, 50% ReductionAMS5225G (Current)6/1/2021
This specification covers an iron-nickel alloy in the form of strip.
AMS F Corrosion Heat Resistant Alloys Committee
Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 psiAS18280H (Current)5/26/2021
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Molded or Extruded Bar, Rod, and Shapes Made from Polyamide-Imide (PAI) Plastic Material Both Filled and Unfilled Grades for High-Impact Strength and Mechanical Strength Applications in High Temperature EnvironmentsAMS3670C (Current)5/19/2021
This specification and its supplementary detail specifications cover molded or extruded bar, rod, and shapes made from filled and unfilled polyamide-imide (PAI) polymer.
AMS P Polymeric Materials Committee
Temporary Protective Coating and RemoverAMS7202 (Current)5/13/2021
This specification establishes requirements for a temporary protective coating (TPC) intended to protect aluminum surfaces from damage and corrosion. This specification also establishes requirements for an alkaline remover used to strip the specified TPCs.
AMS G8 Aerospace Organic Coatings Committee
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Multiple Melted, 1800 °F (982 °C) Solution Heat Treated, Welding Grade Precipitation HardenableAMS5858E (Current)4/27/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Bolts and Screws, Nickel Alloy, UNS N07718 Tensile Strength 185 ksi, Fatigue Rated, Procurement SpecificationAS7466F (Current)3/25/2021
This procurement specification covers aircraft-quality bolts and screws made of corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. The following specification designations and their properties are covered:
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 13Cr - 2.0Ni - 3.0W AnnealedAMS5508G (Historical)3/16/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Elastomer: Rubber, Silicone (VMQ) Non-Oil-Resistant Low Compression Set 65 - 75 Shore A HardnessAMS3307E (Current)3/16/2021
This specification covers a silicone (VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7XXX specification.
AMS CE Elastomers Committee
Elastomer: Methyl Phenyl Vinyl Silicone Rubber (PVMQ) Extreme Low-Temperature Resistant 15 - 30 Type A HardnessAMS3332G (Current)3/10/2021
This specification covers an extreme low-temperature-resistant Methyl Phenyl Vinyl Silicone(PVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7XXX specification.
AMS CE Elastomers Committee
Elastomer: Silicone Rubber (VMQ) Aircraft Piston Engine Oil Resistant Compression Set Resistant 65 - 75 Type A HardnessAMS3357H (Current)3/10/2021
This specification covers a silicone (VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7XXX specification.
AMS CE Elastomers Committee
Fittings, Straight Threaded Boss or Flanged, Fluid Connection, Procurement SpecificationAS4875B (Current)3/9/2021
This SAE Aerospace Standard (AS) establishes the requirements for straight threaded boss or flanged fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion and Heat Resistant Procurement SpecificationAS7471J (Historical)3/1/2021
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered:
E-25 General Standards for Aerospace and Propulsion Systems
Plating, Nickel Low-Stressed DepositAMS2424G (Current)2/26/2021
This specification covers the requirements for electrodeposited low-stressed nickel.
AMS B Finishes Processes and Fluids Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General RequirementsAMS6885/1 (Current)2/23/2021
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Steel, Welding Wire 0.65Si - 1.25Cr - 0.50Mo - 0.30V (0.28 - 0.33C) Vacuum Melted, Environment Controlled PackagingAMS6458K (Current)2/3/2021
This specification covers a low-alloy steel in the form of bare welding wire. Type 2 - copper coated wire was removed from this document (see 8.5).
AMS E Carbon and Low Alloy Steels Committee
Chemical Process Test Specimen MaterialAS2390A (Current)2/1/2021
This standard establishes definitions, guidelines, and requirements governing materials (e.g., alloy and heat treat condition) allowed for use in chemical process test specimens when requirements call for a generic class of alloy.
AMS B Finishes Processes and Fluids Committee
Precipitation Hardenable Steel Alloy, Corrosion and Heat Resistant, Powder for Additive Manufacturing, 15.0Cr - 4.5Ni - 3.5Cu - 0.30NbAMS7021 (Current)11/19/2020
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt%) greater than 40 mesh (425 µm) is allowed.
AMS AM Additive Manufacturing Metals
Bolts, Cobalt-Chromium-Nickel Alloy, UNS R30159, Tensile Strength 260 ksi, Procurement SpecificationAS7475E (Current)11/12/2020
This procurement specification covers bolts made from a corrosion-resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30159.
E-25 General Standards for Aerospace and Propulsion Systems
SCREW, MACHINE - DOUBLE HEXAGON, EXTENDED WASHER HEAD, DRILLED, SILVER PLATED, NICKEL ALLOY (UNS N07001), .1380-40 UNJF-3AAS9712B (Current)9/29/2020
E-25 General Standards for Aerospace and Propulsion Systems
Ethylene Propylene (EPM) Rubber Phosphate Ester Resistant 55 - 65AMS3248D (Current)9/18/2020
This specification covers an ethylene propylene (EPM) rubber in the form of sheet, strip, tubing, molded shapes, and extrusions.
AMS CE Elastomers Committee
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 65Ni - 15.8Cr - 15.2Mo - 0.30Al - 0.05La Consumable Electrode Remelted, Solution Heat TreatedAMS5873G (Current)7/14/2020
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
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, AnnealedAMS5544L (Current)7/14/2020
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion Heat Resistant Alloys Committee
Rings, Flash Welded Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel or Cobalt Alloys, or Precipitation-Hardenable AlloysAMS7490R (Current)7/14/2020
This specification covers flash welded rings made of corrosion and heat-resistant austenitic steels and austenitic-type iron, nickel, or cobalt alloys, or precipitation-hardenable alloys.
AMS F Corrosion Heat Resistant Alloys Committee
Steel, Bars and Forgings 2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C) (HY-180) Double Vacuum Melted Solution Heat Treated, Marage HardenableAMS6543G (Current)6/29/2020
This specification covers a premium aircraft-quality maraging steel in the form of bars 0.50 inch (12.7 mm) and over in nominal diameter or least distance between parallel sides, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Environmental Control System ContaminationAIR1539C (Current)5/29/2020
This SAE Aerospace Information Report (AIR) includes a discussion of liquid and particulate contaminants which enter the aircraft through the environmental control system (ECS). Gaseous contaminants such as ozone, fuel vapors, sulphates, etc. are also covered in this AIR. This publication is concerned with contamination sources which interface with ECS and fuel tank inerting systems, and the effects of this contamination on equipment. Methods of control will be limited to the equipment and interfacing ducting which normally falls within the responsibility of the ECS designer.
AC-9 Aircraft Environmental Systems Committee
Elastomer: Methyl/Methyl Vinyl Silicone (MQ/VMQ) High Temperature Resistant High Strength/Tear Resistant 45 to 55 Type ‘A’ Durometer HardnessAMS3347D (Current)5/26/2020
This specification covers a methyl or methyl vinyl silicone rubber material that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications, use the AMS7000 series specification.
AMS CE Elastomers Committee
Elastomer: Methyl Phenyl Vinyl Silicone (PVMQ) Very Low Temperature/Aircraft Piston Engine Oil Resistant High Strength/Tear Resistant 45 to 55 Durometer Type ‘A’ Hardness For Products in Aircraft Piston Engine Oil/Low Temperature EnvironmentsAMS3345G (Current)5/18/2020
This specification covers a methyl phenyl vinyl silicone rubber material that can be used to manufacture product in the form of sheet, strip, tubing, molded shapes, and extrusions. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the corresponding AMS7000 series specification.
AMS CE Elastomers Committee
Adhesives, Sealants, and Heat Transfer Materials in Battery Systems: A Primer on Materials, Applications, and End-Use Performance RequirementsJ3178_202005 (Current)5/5/2020
This SAE Information Report introduces key concepts and properties of adhesives, sealants, and HTMs and the roles they serve in present-day battery systems applications. The basic chemistry and properties of the three types of materials are summarized along with important health and environmental information. Relevant material dispense methodologies and equipment for material dispensing is reviewed. A series of representative battery applications examples employing adhesives, sealants, and HTMs is also provided with particular attention given to end-use performance.
Battery Systems Adhesives, Sealants and Heat Transfer Matl's
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