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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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...