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MAR-M 302
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Journal Articles
Alloy Digest (1965) 14 (3): Co-43.
Published: 01 March 1965
... MAR-M 302 is a cast cobalt-base alloy having superior oxidation and thermal shock resistance. It was designed primarily for use as a first stage turbine vane to operate in the temperature range of 1500-2000 F. This datasheet provides information on composition, physical properties, hardness...
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MAR-M 302 is a cast cobalt-base alloy having superior oxidation and thermal shock resistance. It was designed primarily for use as a first stage turbine vane to operate in the temperature range of 1500-2000 F. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Co-43. Producer or source: Martin Metals Division, Martin Marietta Corporation.
Journal Articles
Alloy Digest (2012) 61 (10): SA-664.
Published: 01 October 2012
... (13.5 ft) Length: 13 m (42.7 ft) Applications: Mars 190 has been studied for vehicle structures (main battle tanks, armor personal carriers), stationary protection (buildings, sentry boxes, observation posts), and targets. Producer: In USA Industeel USA, LLC Coatesville, PA 19320, USA Tel: (610) 383...
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Mars 190 is a quenched and high tempered armor steel. This datasheet provides information on composition, physical properties, and hardness. It also includes information on forming, heat treating, and joining. Filing Code: SA-664. Producer or source: Industeel USA, LLC.
Journal Articles
Alloy Digest (1965) 14 (7): Co-45.
Published: 01 July 1965
... minutes after pour is recommended to develop optimum elevated temperature proper- ties. MAR-M Alloy 322 is less resistant to oxidation than is MAR-M Alloy 302 alloy, but more resistant than WI-52 alloy. This is particularly true at the higher temperatures above 19000F. Static Oxidation Resistance Time...
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MAR-M Alloy 322 is a cobalt-base casting alloy characterized by exceptional high temperature strength, good ductility, and oxidation resistance throughout its operating range of 1400-2000 F. It is recommended for turbine vanes and blades. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, and machining. Filing Code: Co-45. Producer or source: Martin Metals Division, Martin Marietta Corporation.
Journal Articles
Alloy Digest (2021) 70 (3): SA-869.
Published: 01 March 2021
... comply with MIL-DTL-12560 or EN 10163-2, class Boron 0.003 B, subclass 3. Carbon equivalent(c) 0.85 Iron bal Flatness. The maximum deviation from flatness, measured in accordance with EN 10029, is 3 mm/m (1/8 in. in every 40 in Internal Soundness. Industeel Mars 380 plates are ultrasoni- cally tested...
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Industeel Mars 380 (earlier known as Industeel Mars 190) is a low-carbon, Ni-Cr-Mo-V-B, alloy protection steel that is used in the quenched and tempered condition (typical hardness = 380 HBW). It is used as rolled homogeneous armor for ballistic protection and evaluation of armor-defeating ammunition. This datasheet provides information on composition, hardness, and bend strength. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-869. Producer or source: Industeel France.
Journal Articles
Alloy Digest (1954) 3 (12): SS-22.
Published: 01 December 1954
... Steel) USS 5, Type 501, containing app roximatdy 5% chromium and 5% molybdenum resists corrosion and oxidation at ele- vated temperatures and it is partic&riy adaptable m applications in the petmkum refinery industry where a combination of these proparies and high creep strength and resistance m high...
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USS 5, Type 501, and 5S, Type 502, contain approximately 5% chromium and 0.50% molybdenum. They resist corrosion and oxidation at elevated temperatures and are particularly adaptable to applications in the petroleum refinery industry. Type 502 contains slightly lower carbon and is used for applications where better weldability is required. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-22. Producer or source: United States Steel Corporation.
Journal Articles
Alloy Digest (1954) 3 (8): CI-7.
Published: 01 August 1954
...- of high yield sttength, exceuent weat resm and adapt- abiiiy (0 seleaive hzudenhg comporiti- Toal carbon combiaed cafhon SiliCOll Myrgancse Sulphur s- 2.35-2.75 0.60-0.70 la-l.70 0.35-0.50 0.17 mar. 0.10 max halance Physical Constants Specific gravity, g/cc Density, lb./clL in. Thermal coef. expansion...
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ArmaSteel is a cast ferrous alloy possessing the advantages of high yield strength, excellent wear resistance, and adaptability to selective hardening. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on machining and joining. Filing Code: CI-7. Producer or source: General Motors Corporation.
Journal Articles
Alloy Digest (1957) 6 (5): SS-55.
Published: 01 May 1957
... and slightIy higher totai alloy content, which lessen tbe tendency m weid-embrittiement and enhance the corrosion resiscaaa. ause these types m be preferred over Type 302 for appti- acions involving welding during fabriation. It is not to be inferred, however. that Types 304 or 304L are the proper alloys...
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ARMCO 304 and 304L are the low carbon grades of the 19-9 chromium-nickel stainless steels recommended for welded construction. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-55. Producer or source: Armco Inc., Eastern Steel Division.
Journal Articles
Alloy Digest (1954) 3 (1): Ti-2.
Published: 01 January 1954
...-- Physicul conHan& 0.07 max Density, lIL/aL ilL 0.10 mar. A&dulusofeleseicicy,psi 0.35 max 0.02 max. 2.4 to 3.1 1.2 to 1.8 Imhce94.6 PROPERTIES and forgings It is hut 0.1668 16~,ooo SS 8-10 O.OOOOO5 !E2g 3.0 Table 1 -TYPICAL bGcH4wIcA.L PROPERTIES AzfL Porgings &bH~Uad Bars 140000-165000 135000-160000 120000...
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Ti-150A is a titanium-base alloy containing iron and chromium. It is used primarily in bars and forgings. It is heat treatable and work-hardenable. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-2. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1954) 3 (6): SA-19.
Published: 01 June 1954
... ASTM-WC1 chemical composition creep properties elasticity fracture toughness hardness heat treatability high-temperature alloys joinability machinability physical properties tensile properties Filing Cod.: SA-19 A. S. T. M. - WC1 Steel-Alloy 08 JUNE, 1914 PIGssTd - DATA ON WORLD WIDE...
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ASTM-WC1 is a molybdenum alloy steel recommended for castings for pressure containing parts suitable for high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance as well as heat treating, machining, and joining. Filing Code: SA-19. Producer or source: Alloy steel mills and foundries.
Journal Articles
Alloy Digest (1954) 3 (12): Cu-21.
Published: 01 December 1954
.../cc Density, lb./m. in. Melting range, F. Thermal conductivity, BTU/hftftF. (68OF.) Thermal coef. expansion, h/ixF. (68-572°F.) Specific heat, BTLJ/lbF. ( 68 F. ) Electrical resisrance, mia-ohahcm (20X.) Modulus of elasticiy, psi PROPERTIES MECHANICAL PROPERTIES 8.41 0.304 1630-1650 67 0.0000118...
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NAVAL BRASS is a copper-zinc alloy, containing 3/4% of tin, having high strength, toughness and resistance to corrosion. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cu-21. Producer or source: Brass mills.
Journal Articles
Alloy Digest (1954) 3 (2): Mg-8.
Published: 01 February 1954
... and aausions requihghighfafiguesKengthandgoodaeep Composition2 Nominrl 8.5 0.2 0.5 - 7.8-9.2 0.15 mill 0.2-0.8 0.30 max. 0.05 max. 0.005 mar. 0.005 maz 0.3 max. Physical Constants: specific gn~rp. g/cc Density, Wcu. in. h&king point, F Cohient thermal expansion, F 65-212-P 65-750'F Thermal conducciviy, c&s...
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DOWMETAL O1 is a heat treatable magnesium alloy for forgings and extrusions requiring high fatigue strength and good creep resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, machining, joining, and surface treatment. Filing Code: Mg-8. Producer or source: The Dow Chemical Company.
Journal Articles
Alloy Digest (1954) 3 (7): Al-18.
Published: 01 July 1954
... righr castings. bnpusition: ZzE . ? E- chromitlm Titanium Otha demerits, each orher eiemalrs, total 1.0-1.5 4.5-5.5 0.4-0.6 0.6 max. 0.50 max 0.30 max. 020 max. 020 max. 0.05 mar. 0.15 max. Remainder Physiii constantsz specific gravity, g/cc Density, h/at in. kEZEZZ&ty, 70 Cu Thermal conduaiviy, caI/sec...
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ALUMINUM 355 is a heat treatable aluminum alloy containing silicon and copper as the major alloying elements. It is recommended for light weight, high strength, pressure tight castings. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as heat treating, machining, and joining. Filing Code: Al-18. Producer or source: Aluminum Company of America.
Journal Articles
Alloy Digest (1967) 16 (11): SS-202.
Published: 01 November 1967
.... Composition: Physical Constants: Carbon 0.08 max. Manganese 2.00 mar. Sulphur 0.030 max. Phosphoms 0.030 max. SiIicon 0.75 max. Chromium 16.00-18.00 Nickel 11.00-14.00 Molybdenum 2.00-3.00 Iron Remainder Density, lb/cu.in. Thermal conductivity, Btu/ft2/in/br/OF at 21PF Thermal coef. expansion/OF r 10-6 75...
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Croloy 16-13-3 is a molybdenum-containing 18-12 type austenitic stainless steel having better corrosion resistance than the 18-8 type stainless steels. It is recommended for corrosion resisting applications in the chemical and oil refinery industries, paper pulp processing, etc. In addition to corrosion resistance, this alloy is characterized by superior resistance to creep at elevated temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-202. Producer or source: Babcock & Wilcox Company.
Journal Articles
Alloy Digest (2023) 72 (5): CS-247.
Published: 01 May 2023
... at the surface of a 1045 round bar in the quench hardened condition (water quenched from 900 °C, or 1650 °F) showing low-carbon and high-carbon martensite. The hardness at the surface of the bar is 743 HV, while the hardness in the center is 596 HV. These micrographs were from an area containing nearly 100% mar...
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1045, 1045H, 1046, C45, C45E, and C45R are wrought medium-carbon (carbon = 0.42–0.51%) non-alloy steels that are used in the normalized, cold worked, or quenched and tempered condition. 1045, 1045H, 1046, C45E, and C45R may also be flame or induction hardened, nitrided, or nitrocarburized. These steels are widely used for moderately and highly stressed parts that require higher strength levels than can be achieved by the lower carbon grades, and where the expense of an alloy steel is not justified. Owing to their low hardenability their use in the quench hardened and tempered condition is not recommended for large sizes as the improvement in mechanical properties over the normalized condition is insufficient to justify the additional cost of heat treatment. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming and heat treating. Filing Code: CS-247. Producer or source: Heat Treater's Guide.
Journal Articles
Alloy Digest (2023) 72 (8): CS-257.
Published: 01 August 2023
... and martensite content on the as-quenched hardness Carbon wt% 0.46 0.48 0.50 0.52 0.54 Hardness, in HRC, for a martensite (M) content of 99.9% M 95% M 90% M 80% M 50% M 59.1 55.2 52.7 49.0 45.1 60.0 56.0 53.5 49.8 46.0 60.9 56.8 54.3 50.6 46.8 61.7 57.5 55.0 51.3 47.7 62.5 58.2 55.7 52.0 48.5 Source: Ref 48 (p...
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1049 is a wrought medium-carbon (carbon = 0.46-0.53%) non-alloy steel that is used in the normalized, cold worked, or quenched and tempered condition. 1049 may also be flame or induction hardened, nitrided, or nitrocarburized. This steel is widely used for moderately and highly stressed parts that require higher strength levels than can be achieved by the lower carbon grades, and where the expense of an alloy steel is not justified. Owing to its low hardenability, its use in the quench hardened and tempered condition is not recommended for large sizes, as the improvement in mechanical properties over the normalized condition is insufficient to justify the additional cost of heat treatment. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming and heat treating. Filing Code: CS-257. Producer or source: Heat Treater’s Guide.