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Hastelloy alloy X

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Journal Articles
Alloy Digest (1954) 3 (12): Ni-14.
Published: 01 December 1954
... HASTELLOY Alloy X is a nickel-chromium-iron-molybdenum alloy recommended for high-temperature applications. It has outstanding oxidation resistance at high temperatures under most operating conditions, and good high-temperature strength. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1985) 34 (8): Ni-320.
Published: 01 August 1985
... *Nominal compositions in 70: HAYNES 188: 40 Co, 22 Cr, 22 Ni and 14.5 W. HASTELLOY X: 49 Ni, 22 Cr, 9 MO, 15.8 Fe and 1.5 max. Co. Alloy HAYNES 230 HAYNES 188 HASTELLOY X *Test conditions: Metal Total Metal Affected Loss (Loss + max. pene- mils/ side tration) mils/ side 3.6 7.7 8.0 11.3 15.4 19.5 Burner...
Journal Articles
Alloy Digest (1987) 36 (6): Fe-76.
Published: 01 June 1987
.... cycling to room temperature every 168 hours.) 1800°F 2000°F Average** Avera.ge*+ Metal Metal Metal Metal Loss Affected Loss Affected Alloy (mils) (mils) (mils) (mils) HASTELLOY alloy X 0.3 0.9 I.5 HAYNES alloy No. 556 0.4 I. I 1.0 INCONEL alloy 601 0.5 I.3 I.2 HAYNES alloy No. 800H AISI Type 446 Stainless...
Journal Articles
Alloy Digest (1987) 36 (11): Ni-353.
Published: 01 November 1987
... RT 47.3 35.5 56.9 90.3 Base 1600°F 40.0 33.7 59.8 92.3 Base 1600°F HASTELLOYQ alloy X to 113.2 57.0 51.7 54.0 Base RT HASTELLOY@ alloy X 113.6 58.2 52.6 55.6 Base RT 40.1 32.9 41.8 71.0 Base 1600°F 44.7 33.7 35.8 58.6 Base 1600°F HAYNES@ alloy 188 to 129.0 76.3 21.1 33.7 In Weld RT HAYNES@ alloy 188...
Journal Articles
Alloy Digest (1971) 20 (4): Co-63.
Published: 01 April 1971
... Layer that forms on the surface is adherent and has a high melting point. MAR-M 9 18 has approximately the same resistance to static air oxidation as nickel-base Hastelloy alloy X and is markedly superior to cobalt-base alloy L 605. Comparative rates of oxidation at 21000F for the three materials...
Journal Articles
Alloy Digest (1986) 35 (8): Ni-336.
Published: 01 August 1986
... (980°C). Comparable carbon pickups for HASTELLOY* ALLOY X were 0.52, 1.75. and 2.5 mg/cmz. respectively. Chlorination: Limited test results (8 hours exposure) at 1650 F (900°C) show HAYNES ALLOY No. 214 to have the best resistance of all alloys tested. to both oxidizing and reducing atmospheres...
Journal Articles
Alloy Digest (1985) 34 (9): Ni-322.
Published: 01 September 1985
... 400 204 800 427 IO00 538 Yield Strength Elongation Reduction Tensile Strength (0.2% Offset) (2 in.) of Area psi (MPa) psi (MPa) 9% 9% 100000 (689) 46000 (3 17) 64 77 85000 (586) 38000 (262) 69 65 76000 (524) 28000 ( 193) 75 71 7 1 ooo (490) 25000 ( 172) 75 66 0.297 8.22 7.7 x IO-6 8.3 x IO-6 8.9 x 10...
Journal Articles
Alloy Digest (1964) 13 (5): Ni-91.
Published: 01 May 1964
...: AISI No. 680 Hastelloy alloy X AMS 5754D (bar, solution created) AMS 5536C (sheet, solution treated) AMS 5798 (wire, cold drawn) AMS 5799 (coated welding electrodes) U.S. Pat. No. 2, 703, 277 Union Carbide Corp. General Characteristics: Unitemp-HX is a nickel-base high temperature alloy. Additions...
Journal Articles
Alloy Digest (1988) 37 (12): Ni-365.
Published: 01 December 1988
... Elongation Strength (02% Offset) (2 in.) psi 0 psi NW 5 l/8 in. sheet Annealed I~CIW 54ooo( 372) 57 3 l/2 x 0.250 59% cold inchtube WOlkCd 168ooo (1157) 15oow (1034) 14 0.30 8.3 7.7 x 10-6 70 28x106 Heat Treatment: HASTELLOY alloy H-9Mis a solid solution strengthened alloy and is not heat-treat hardenable...
Journal Articles
Alloy Digest (1971) 20 (5): Ni-164.
Published: 01 May 1971
... 94000 34000 87000 33000 64000 30000 39000 27000 % 56 55 2; 77 49 49 70 71 75 73 92 127 0.321 8.90 24 15-2500 6.2 x 10-6 7.4 x 10-6 8.8 x lo-6 2: 71 132 159 195 779 0.102 29.8 x 106 25.5 x 106 DOI: 10.31399/asm.ad.ni0164 Copyright © ASM International® 1996 Tabte 3 - CREEP PROPERTIES OF 0.094-m. SHEET...
Journal Articles
Alloy Digest (1974) 23 (11): Ni-211.
Published: 01 November 1974
...) (At 12000F) (At 1800°F) *Condition: 1950oF, rapid quench. Triplicate tests. PROPERTIES 0.312 8.64 See Table 1 See Table I 6.0 x 10-6 7.4 x 10-6 8.7 x 10-6 30.8 x 106 28.3 x 106 25.0 s 106 20.6 s 106 Table 1 - SOME PHYSlCAL PROPERTIES Temperature, oF 32 74 212 392 572 752 932 1112 Specific heat, Btu/Ib...
Journal Articles
Alloy Digest (1985) 34 (7): Ni-317.
Published: 01 July 1985
...) 2475-2550 Thermal conductivity, Btu/ftz/in./hr/ OF (At 118OF) (At 212oF) 0.314 8.69 (1367-1399) 0.099 414 44.8 6.9 x 10-6 7.4 x 10-6 8.8 x 10-e 70 77 (At 572OF) 108 (At 932 F) 148 Modulus of elasticity, psi (At 70°F) 29.9 x 106 (At 1800°F) 21.1 x 106 PROPERTlE8 Heat Treetment: HASTELLOY alloy C-22 can...
Journal Articles
Alloy Digest (1993) 42 (8): Ni-440.
Published: 01 August 1993
... resistivity, ohms/& mil ft Specific heat, Btu/lb/ F Modulus of elasticity, psi (dynamic) 0.321 8.90 2415-2500 6.2 x lo-6 7.4 x lad 8.8 x lo-6 50 65 71 132 159 195 779 0.102 Nickel Bal. Bal. *Maximum PROPERTIES Table 1 - TYPICAL ALL WELD METAL TENSILE DATA* Room temperature 29.8 x 106 1OOO F 25.5 x lob Welding...
Journal Articles
Alloy Digest (1977) 26 (9): Ni-249.
Published: 01 September 1977
... max. 1.00 max. 26.00-30.00 2.00 max EXE 0102 max: 0.040 max. 0.030 max. Remainder 0.333 9217 See Table 1 See Table 4 2-z ; $16 6:s x 10-6 31.4 x 106 Modulus of elasticity, psi (Dynamic) (At ?2W (At 6OOoF) (At 8OoOF) (At 1000°F) 29.3 x 106 28.4 x 106 27.4 x 106 PROPERTIES Table 1 - SOME PHYSICAL...
Journal Articles
Alloy Digest (1993) 42 (4): Ni-425.
Published: 01 April 1993
...) (At 800°F) (At 1000°F) Molybdenum 26.0-30.0 26.0-30.0 Tungsten 1.0* l.o* others 0.W 0.50* Nickel Bal. Bal. PROPERTlES *Maximum Table 1 - SOME PHYSICAL PROPERTIES 0.333 9217 See Table 1 See Table 1 5.7 x l&6 6.2 x 106 6.5 x lad 31.4 x 106 29.3 x 106 28.4 x 106 27.4 x 106 Temperature, OF 32 212 392 572 752...
Journal Articles
Alloy Digest (1960) 9 (2): Ni-55.
Published: 01 February 1960
... coef. expansion/ F x lo-6 0.5 max. 70- 400°F 5.76 Boron 0.01 max. 70-1800°F 8.32 Sul hur Ni 2 el 0.03 max. Thermal conductivity, Remainder Bti~?2<iF 0 66.7 at 1292°F 217.7 Specific heat, Btu/lb/ F at 212°F 0.095 * The term Hastelloy is a registered trade-mark of Union Carbide Corporation. PROPERTIES...
Journal Articles
Alloy Digest (1973) 22 (1): Ni-184.
Published: 01 January 1973
... EXPANSION Tdde 2 -THERMAL CONDUCTIVITY AND SPECIFIC HEAT Temperature Range Coefficient Test Temperature Thermal Conductivity Specific Heat oF Per oF OF Btu/sq ft/hr/oF/in. BWWF 68-200 6.4 x lo-6 32 97 0.095 68-1000 0.107 68-1200 E 392 152 124 0.114 68-1600 8.2 1112 146 0.119 68-2000 89 1472 181 0.141 1652...
Journal Articles
Alloy Digest (1993) 42 (2): Ni-423.
Published: 01 February 1993
... route. CW = Cold Worked Table 7 - SLOW STRAIN RATE TEST (SSRT) DATA COMPARISON OF SSRT BETWEEN G-50m ALLOY AND ALLOY G-3 Envimnment - 25% NaCl + 0.5% Acetic Acid + I&S (100 psi). Extension mte - 4 x l@/sec Time E/Tim A alloy G-3 G-50 alloy (300°F) (350°F) Average 0.95 1.11 Minimum 0.72 O.% 1.16 1.32...
Journal Articles
Alloy Digest (1965) 14 (1): Ni-97.
Published: 01 January 1965
...) Specific gravity Density, lb/cu.in. Electrical resiscivicy, microhm-cm Thermal coef. expansion, in/in/OF x lo-6 76- 212 F 76- 752°F 76-12920F 76-2095°F Thermal conductivity, Btu/ft2/in/oF/hr 700F 1: 12OOoF at 20000F Specific hear, Bcu/lb/oF at 1OOOoF Modulus of elasticity, psi x 106 at 2OOOoF PROPERTIES...
Journal Articles
Alloy Digest (1996) 45 (9): Ni-516.
Published: 01 September 1996
... + 42 @L Fe?(sO&. boiling (b)G28B: 23% l-X+0, + 1.2% Ha + l%Fca,+l%CuucI,boiling Table 3 Localized Corrosion Resistance C-2000 110 230 C-2000 95 203 G276 105 221 C-276 60 140 C4 90 194 C-4 50 122 Table 4 Stress-Corrosion Cracking Resistance 45% MgcI, 1WC GOPW w limembhrrb Gmoo C-276 2oCB-3 316L.s hWWn...