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  • Properties

    OF SOME METALS

    AND ALLOYS

    INTRODUCTION

    The information assembled in this publication has been obtained from one ormore of various sources. The chemical compositions and the mechanical andphysical properties are typical for the metals and alloys listed.These nominal data are presented to facilitate general comparison and are notintended for specification or design purposes. Variations from these typical valuescan be expected which will be dependent upon mill practice, and materialsrespective to form and size. Strength is generally higher, and ductility correspond-ingly lower, in the smaller sizes of rod and bar materials and in cold-drawn wire;the converse is true for the larger sizes. In the case of heat-treated carbon andstainless steels, mechanical properties and hardnesses vary widely with the par-ticular heat treatment used.

    REFERENCES

    Many of the alloys listed in the publication are marketed under certain wellknown trademarks of their producers, and an effort has been made to associatesuch trademarks with the applicable materials listed herein. Such trademarks,together with their proprietors, are listed on page 62.Specifications, mainly those published by the American Society for Testing andMaterials, are shown for many of the materials. Other specifications may alsobe available. Where specifications appear, their latest date of issue should apply.Sources of additional information, concerning properties and specifications areshown on page 63.While this listing and other data were compiled from sources believed reliable,possible errors and/or omissions may exist. We would welcome corrections orsuggestions. Therefore, this guide may be revised periodically to have it asaccurate as possible with up-to-date information.

  • IN D EX

    9% Nickel Steel1212 Stainless Steel155 PH* Stainless Steel.16256 Alloy174 PH* Stainless Steel ..177 PH* Stainless Steel.1714 Cu Mo* Stainless Steel ..189 LW* Stainless Steel.18K White Gold199 DL Alloy199 DX Alloy2169 Stainless Steel3520 bal Fe Alloy.42% Ni Fe Alloy.49% Ni Fe Expansion Alloy ...49% Ni Fe Magnetic Alloy .6015 bal Fe Alloy ..794 Ni Mo Alloy.8020 Ni Cr Alloy.200 ALLOY*300M Alloy Steel901 Alloy713C Alloy713LC AlloyA286 Alloy

    ~C~OMr ~Alnico Alloys (Permanent Magnet Alloys)

    II. III. IV. V. VI.. 20VII. VIII . .. . .... 22

    Aluminum AllOYS, Wrought1100 & 2017 12Alclad 2024. 3003. 5052. 6061

    & 7075 14Aluminum Alloys, Cast

    13. 43. A132. 142. 195. 214. 220& 380 14

    AM350* Stainless Steel 48AM355* Stainless Steel 48AM363* Stainless Steel 50Antimony 10

    B1900 Alloy 36Bismuth-Lead Alloy 10BiPbSnCd Alloy 12BiPblnCdSn Alloy 12Bismuth-Tin Alloy 10Brass

    Admiralty (CA443. 444 & 445) . 6Cartridge (CA260) 6Leaded Red (83-4-6-7) . . . . . . . . 8Leaded Red (85-5-55) 8Naval (CA464) 6Red (CA230) 6Yellow (CA270) 6

    BronzeAluminum (CA614) 8Architectural (CA385) 6Commercial (CA220) . 6G (88-10-2) 8High Silicon (CA655) 8Leaded Tin (83-7-7-3) 10

    ., See page 62 for list of trademarks.

    4

    Page38464838484850486050505020222220202020203832323234

    PageM (888-4) . . . . . . . . . . . . . 10Manganese (CA675) 8Nickel Tin. Type A. . . . . . . . . 10Nickel Tin, Type B. . . . . . . . . . 10Phosphor (CA510) 6Phosphor (CA524) 8

    CARPENTER* No. 10 . . . . . . . .. 46CARPENTER* No. 20 46CARPENTER* 20Cb3 46Cast Iron Alloys (See Iron. Cast)ColumbiumColumbiumTantalumTungsten AlloyColumbiumVanadium AlloyColumbiumZirconium AlloyControlled Expansion AlloysCopper Alloys, Wrought

    CA110 (Copper) .CA170 (Copper Beryllium)CAl72 (Copper Beryllium)CA175 (Copper Beryllium)CA210 (Gilding Metal)CA220 (Commercial Bronze)CA230 (Red Brass)CA260 (Cartridge Brass) .CA270 (Yellow Brass)CA280 (Muntz Metal)CA385 (Architectural Bronze)CA443 (Admiralty Brass) .CA444 (Admiralty Brass)CA445 (Admiralty Brass) .CA464 (Naval Brass) .CA510 (Phosphor Bronze)CA524 (Phosphor Bronze) .CA614 (Aluminum Bronze)CA655 (High Silicon Bronze).CA675 (Manganese Bronze)CA706 (Copper Nickel. 90-10+Fe).CA715 (Copper Nickel. 70-30+Fe).CA735 (Nickel Silver)CA752 (Nickel Silver)CA766 (Nickel Silver)CA770 (Nickel Silver)

    Copper Beryllium AllOySCA170. CAl72 & CA175.Copper Beryllium 50

    Copper.Nickel AlloysCA706 & CA715(55-45) .Castings

    CunicoCunifeCUSTOM 455* Stainless Steel.

    88

    ... ..... 10222248

    D979 Alloy . . . . . . . . . . . . . . . . . . 36DISCALLOY* 38DURANICKEL * alloy 301. 24Ductile Irons 40DURIRON* 42DURICHLOR* 42

    EVANOHM* 20

    GMR 235DGilding Metal (CA210)Gold

    Pure18K WhiteW.E. No.1

    5858585822

    66666666666666668888888888

    PageGreek Ascoloy Stainless Steel. . . . . . . .. 50

    HASTELLOY* alloysB. C, D, F. G. N. . . . . . . . . . . . 30W, X. & R-235. . . . . . . . . . . 32

    Heat Resisting Alloys, CastHA. HC 54HD. HE. HF. HH. HI, HK, HL. HN. HT.

    HU. HW & HX. . 56High Temperature-High Strength Alloys. 34

    IN 100 Alloy 34IN 102 Alloy. . . . . . . . .. 34INCOLOY* nlckel-lron-chromlum alloys

    800. 802 & 825INCONEL * nickel-chromium-iron alloys

    600, 625. 718. X750 & 751.Ingot IronINVAR*IridiumIronCrAI AlloyIron, Cast

    Cast GrayDuctileMalleableNi-Hard, Types 1. 2 & 4.Ni-Resist, Type 1Types 2. 5. D2 & D5.Iron-Silicon Alloy (DURIRON*)Fe-Si-Mo Alloy (DURICHLOR*) ..

    Iron, Wroughtlron-Nickel Temperature Compensating

    Alloys .ISOELASTlC* .

    KANTHAL*KARMA*KOVAR*

    66

    L605 AlloyLead

    Pure .AntimonialTellurium

    326

    M252 AlloyMagnesium Alloys

    AZ 31B & AZ 80A .AZ 91A & AZ 91B ..AZ 91C & AZ 92A.EZ 33A & HK 31A.HZ 32A & ZK 60A.

    Magnetic AlloysMalleable Iron .Manganese Alloy 772Maraging Steels

    18-20018-250 & 18-300

    MARM246 AlloyMolybdenumMolybdenum-V:! Ti AlloyMOlybdenum-2.5 (Ni+Cu) AlloyMolybdenum-7.5 Ni-2.5 Cu Alloy.MONEL * nickel-copper alloys

    400. 401. 404. R405 & K-500.410 (Cast) & 505 (Cast)

    Mu MetalMuntz Metal (CA280)

    606060

    28

    2838226020

    404040424042424238

    2222

    202022

    34

    121212

    34

    1616161616204012

    38403458585858

    2626206

  • 24.. ' 24

    .......... 242424242436

    N-155 AlloyNickel Alloys

    200, 201, 205, 211 & 270 ..Cast Nickel .Nickel Beryllium 440Nickel Beryllium M220CNickel Beryllium Cr-1 .OURANICKEL * alloy 301PERMANICKEL* alloy 300TO Nickel .

    Nickel-Chromium AlloysSO-20 .60-15 + Fe35-20 + Fe .

    Nickel-Chromium-Aluminum AlloyNickel-Molybdenum Alloy (79-4)Nickel-Iron Alloy (49% Ni)

    Expansion AlloyMagnetic Alloy

    Nickel-Iron-Cobalt AlloyNickel Silver Alloys, Wrought

    CA735, CA752, CA766 & CA770.Nickel Silver AllOYS, Cast ..Ni-Hard Cast Irons

    No. I, No.2 & No.4.NIKROTHALNIMONIC nickel-chromium alloys

    75, SOA, 90 & 115 ..NI-SPAN C .Non-Galling Alloys

    WAUKESHA METAL* No. 23.WAUKESHA METAL * No. SS.

    Ni-Resist Cast IronsType 1Types 2 & 5.Types 02 & 05.

    Permanent Magnet AlloysPERMANICKEL" alloy 300 .

    PH 15-7 Mo Stainless Steel ..PH 14-8 Mo Stainless Steel.PH 13-8 Mo Stainless SteelPalladiumPalladium Alloy 934Palladium-Ruthenium AlloyPalladium-Silver Alloy .PlatinumPlatinum-Iridium AlloyPlatinum-Rhodium AlloyPlatinum-Rubidium AlloyPrecious Metals & Alloys

    See page 62 for list of trademarks.

    Page38

    PageRefractory Alloys . . . . . . . . 58RENE 41 alloy . . . . . . . . . . . . . . . . . .. 34Resistance Heating Alloys 60Rhodium '.' .. 20RODAR'" 22Ruthenium 60

    5252525454

    ....... 54

    S-816 AlloySAE 1020 SteelSilver

    CoinFineSterling .

    Silver Brazing AlloysEASY-FLO*R-T Alloy

    Solder50-50 (Sn-Pb)60-40 (Sn-Pb)

    Stainless Steel, CastCA-15, CA-40 & CB-30.CC-50, CE-30 & CF-3.CF-S, CF-3MCF-SM, CF-SC, CF-16F & CF-20.CG-SM, CH-20 & CK-20 ..CN-7M & CO-4MCu

    Stainless Steel, WroughtType 201Types 202, 301, 302, 303 & 303Se.Types 304, 304L, 305, 309 & 310 ..Type 304 +BoronTypes 314, 316, 316L & 317.Types 321, 330 & 347.Types 405, 410, 414 & 420.Types 430, 431, 440C & 446.12-1215-5PH*, 17-4PH* & 17-7PH*.17-14Cu Mo"IS-9LW"19-90L & 19-90X .21-6-9AM350* & AM355*AM363*CARPENTER" No. 10CARPENTER' No. 20 .CARPENTER' 20Cb-3.CUSTOM 455* ..Greek AscoloyPH 15-7Mo*, PH 14-SMo* &

    PH 13-SMo" 48STAINLESS "W'" 48

    2020202020

    222022

    810

    4220

    3022

    2426

    404242

    24484848606060606060606060

    0

    '3638

    424444444646505246485048505048504646464850

    606060

    IN 0 EX

    PageSteel, Alloy

    9% Nickel .300 M .Maraging IS-200 .Maraging lS-250Maraging lS-300

    Steel, Carbon, SAE 1020

    38383840

    ............ 4038

    6060 Tantalum

    TO Nickel .THERLOTinTitanium Alloys

    Ti-35A & Ti-50A 16Ti-75A & Ti-0.2 Pd 18Ti-5AI-2.5Sn . . . . . . . . . . . . .. 18Ti-SAI-IMo-IV 18Ti-6AI-2.5Sn-4Zr-2Mo 18Ti-6AI-6V-2Sn . . . . . . .. 18Ti-6AI-4V 18Ti-13V-11Cr-3AI 18

    Tungsten . . . . . . . . . . . . . .. 58Tungsten-Rhenium Alloys 58

    58362212

    1212

    UDIMEP alloy 500UDIMET* alloy 700Uranium

    363658

    WASPALOY* ."WAUKESHA METAL*

    No. 23 .No. SS

    White Gold, 18KWI-52 AlloyWrought Iron .

    36

    2426603638

    X-40 Alloy 38

    ZILLOY-15ZincZinc-Aluminum AlloyZinc-AI-Cu-AlloyZirconiumZirconium-Hafnium Alloy

    121212125858

    o

    5

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brineli or

    Material % Condition 1000 psi 1000 psi % . Rockwell

    COPPER AND COPPER ALLOYSCopper CA 110 Strip Annealed 10& 32 45 RF'IO

    Sheet-ASTM B 152 Cu -99.90 minRod-ASTM B 124, B 133 Spring Temper 50& 55 4 RB60Wire---ASTM B 1, B 2, B 3

    Copper Beryllium CA 170 Cu-bal Strip Annealed plus age 145 165 7 Rc35Strip---SAE CA 170 Be- 1.7

    Co- 0.25 Hard plus age 170 190 3 Rc40

    Copper Beryllium CA 172 Cu-bal Strip Annealed plus age 150 175 6 Rc38Sheet & Strip---ASTM B 194 Be- 1.9Wire---ASTM B 197 Co- 0.25 Hard plus age 180 200 2 Rc42Rod-ASTM B 196

    Copper Beryllium CA 175 Cu-bal Annealed plus age 90 110 11 RB96Rod-SAE CA 175 Be- 0.60

    Co- 2.5 Hard plus age 110 120 8 RB99

    Copper Beryllium 50 Cu-bal Bar Annealed plus age 90 110 17 RB96Be- 0.38Co- 1.55 \4 Hard plus age 110 120 14 RB99Ag- 1.00

    Gilding Metal CA 210 Cu-95 Strip Annealed 108 34 45 RF'16Plate, Sheet, Strip, Bar-ASTM B 36 Zn- 5

    Spring Temper 58& 64 4 RB73

    Commercial Bronze CA 220 Cu-9o Strip Annealed 10& 37 45 RF53Plate, Sheet, Strip, Bar-ASTM B 36 Zn-lOWire-ASTM B 134 Spring Temper 62& 72 3 RB78

    Red Brass CA 230 Strip Annealed 15& 40 50 50Strip, Sheet, Plate---ASTM B 36 Cu-85Wire---ASTM B 134 Zn-15 Hard Temper 60& 75 7 135Tube---ASTM B 135

    Cartridge Brass CA 260Sheet-ASTM B 19 Cu-7o Strip Annealed 11& 44 66 RF54Plate---ASTM B 36 Zn-3oWire-ASTM B 134 Spring Temper 65& 94 3 RB91Tube---ASTM B 135

    Yellow Brass CA 270 Cu-65 Strip Annealed 14& 46 65 RF58Strip, Sheet, Plate---ASTM B 36 Zn-bal

    Spring ifemper 62& 91 30 RB90

    Muntz Metal CA 280 Cu-61 Annealed 21& 54 45 RFSOTube---ASTM B 135 Zn-balTube---ASTM B 111 \4 Hard 50& 70 10 RB75

    Architectural Bronze CA 385 Cu-balZn-40 As Extruded 20& 60 30 RB65Pb- 3.0

    Admiralty Brass CA 443, CA 444, CA445 Cu-71Plate---ASTM B 171 Zn -bal Annealed 22& 53 65 RF75Tube---ASTM B 111 Sn- 1

    As, Sb or p-0.06

    Naval Brass CA 464 Cu-60.5 Annealed 25& 58 49 RB56Rods, Bars & Shapes-ASTM B 21 Zn-bal

    Sn - 0.75 \.i Hard 58& 70 17 RB75Phosphor Bronze CA 510 Cu-bal Annealed 19& 47 64 RF73

    Sheet-ASTM B 103 Sn- 5Rod-ASTM B 139 P - 0.2 Spring Temper 80& 100 4 RB95Wire---ASTM B 159

    &=0.5% Extension

    6

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10- Btujsq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbj"F in.jinpF /hr j"F fin. /cir mil It in 10 psi x 10 psi Material

    COPPER AND COPPER ALLOYS0.322 8.91 1980 0.092 9.41 25123 10.3 17 6.4 Copper

    CA 1109.82

    0.298 8.26 1600 to 1800 9.3 7503 to 900 39 Copper BerylliumCA 170

    0.298 8.26 1600 to 1800 0.10 9.3 7503 to 900 39 19 7.3 Copper BerylliumCA 172

    17 6.5

    0.316 8.75 1885 to 1955 9.84 14503 to 1800 20 Copper BerylliumCA 175

    0.316 8.75 1850 to 1900 9.82 15003 to 1700 19 Copper Beryllium50

    0.320 8.86 1950 0.09 10.02 16203 18.5 17 6.4 Gilding MetalCA 210

    0.318 8.80 1910 0.09 10.22 13083 23.6 17 6.4 Commercial BronzeCA220

    0.316 8.75 1880 0.09 10.42 11043 28 17 6.4 Red BrassCA230

    Cartridge Brass0.308 8.53 1750 0.09 11.12 8403 37 16 6.0 CA 260

    Yellow Brass0.306 8.47 1710 0.09 11.32 8043 38.4 15 5.6 CA 270

    Muntz Metal0.303 8.39 1660 0.09 11.62 8523 37 15 5.6 CA280

    Architectural0.306 8.47 1630 0.09 11.62 8523 37 14 5.3 BronzeCA 385

    Admiralty Brass0.308 8.53 1720 0.09 11.22 7683 41.5 16 6.0 CA 443CA 444

    CA 445

    Naval Brass

    0.304 8.41 1650 0.09 11.82 804 39.9 15 5.6 CA 464

    0.320 8.86 1920 0.09 9.92 4803 69.1 16 6 Phosphor BronzeCA 510

    1=68 to 212 F 2=68 to 572 F 3=ot 68 F 4=68 to 392 F

    7

  • Properties OF SOM E METALS AN 0 ALLOYSTypical Mechanical Properties

    Material

    Nominal Composition(essential elements),

    %Form andCondition

    YieldStrength

    (0.2% offset),1000 psi

    TensileStrength,1000 psi

    Elongationin 2 in.,

    %

    Hardness,Brinell orRockwell

    co P PER AN D CO P PER ALLOYS (continued)Phosphor Bronze CA 524

    Sheet-ASTM B 103Rod-ASTM B 139Wire-ASTM B 159

    Cu-balSn-lOP - 0.2

    Annealed 66

    122

    68

    Spring Temper 4

    Aluminum Bronze CA 614Sheet-ASTM B 169Rod-ASTM B 124, B 150

    Cu-balAI- 7Fe - 2.5

    Soft 82

    89

    40

    32Hard

    High Silicon Bronze CA 655Sheet-ASTM B 96, B 97Rod-ASTM B 98, B 124Wire-ASTM B 99

    Annealed 56

    110

    63

    4Cu-balSi - 3.3 Spring Temper

    Manganese Bronze CA 675Bar, Rod& Shapes-ASTM B 138

    Cu-58.5Zn -balFe - 1.4Sn- IMn- 0.3

    Rod Soft 65 33

    Yz Hard 84 19

    Copper-Nickel CA 706Tube-ASTM B 111Plate-ASTM B 171

    Cu-balNi -10Fe- 1.25Mn- 0.3

    Tube Annealed 44 42

    Light Drawn 60 10

    Copper-Nickel CA 715Sheet-ASTM B 122Plate-ASTM B 171Tube-ASTM B 111

    Cu-balNi -30Fe- 0.55Mn- 0.5

    Tube Annealed 60 45

    Copper-Nickel(55-45)

    Cu-55Ni -45

    Annealed 60

    135

    32 80

    Cold Worked 250

    Nickel Silver CA 735Sheet, Strip, Plate-ASTM B 122 No. I

    Cu-72Zn -balNi -18

    Soft 22a 55

    78

    40

    5

    RB35

    Hard RB85

    Nickel Silver CA 752Sheet, Strip, Plate-ASTM B 122 No.2

    Cu-65Zn -balNi -18

    Annealed

    Hard

    58

    85

    40

    3

    RB40

    RB87

    Nickel Silver CA 766 Cu-56.5Zn -balNi -12

    Soft 60

    97

    40 RB45

    Hard RB88

    Nickel Silver CA 770(Wrought)Sheet, Strip, Plate-ASTM B 122 No.4

    Rod & Bar-ASTM BI51Wire-ASTM B 206

    Cu-55Zn -balNi -18

    Annealed 60 40 RB55

    Hard 100 3 RB91

    Leaded Red Brass(85-5-5-5)Castings-ASTM B 145

    Cu-85Zn- 5Pb- 5Sn- 5

    As Cast 35 25 60

    Leaded Red Brass(83-4-6-7)Castings-ASTM B 145Alloy 4B

    Cu-83Zn- 7Pb- 6Sn- 4

    As Cast 34 24 55

    G Bronze(88-10-2)Castings-ASTM B 143Alloy IA

    Cu-balSn-lOZn- 2

    As Cast 45 31 80

    R=O.5% Extension

    8

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb;oF in./inpF /hr;oF fin. /cir mil ft in 106 psi x 106 psi Material

    COPPER AND COPPER ALLOYS (continued)0.317 8.78 1830 0.09 10.22 3483 94.3 16 6 Phosphor Bronze

    CA 524

    0.285 7.89 1915 0.09 9.02 4683 74.1 17 6.4 Aluminum BronzeCA 614

    0.308 8.53 1880 0.09 10.02 2523 148 15 5.6 High SiliconBronzeCA 655

    Manganese Bro'nZe0.302 8.36 1630 0.09 11.82 7323 43.2 15 5.6 CA 675

    0.323 8.94 2100 0.09 9.52 3123 115 18 6.8 Copper NickelCA 706

    CopperNickel0.323 8.94 2260 0.09 9.02 2043 225 22 8.3 CA 715

    0.321 8.89 2355 8.28 155 300 24 CopperNickel(5545)

    0.319 8.82 2100 Nickel SilverCA 735

    0.316 8.73 2030 0.09 9.02 2283 173 18 6.8 Nickel SilverCA 752

    0.310 1832 2643 189 Nickel SilverCA 766

    Nickel Silver0.314 8.70 1930 0.09 9.32 2043 189 18 6.8 CA 170

    Leaded Red Brass0.317 8.75 1840 10.2 500 63 13 (85-5.5-5)

    Leaded Red Brass0.312 8.64 1800 (83-4-6-7)

    G Bronze0.315 8.72 1800 15

    2=68 \0 572 F 3=0\ 68 F

    9

  • Properties OF SOM E METALS AN D ALLOYS

    Material

    Typical Mechanical Properties

    Nominal Composition(essential elements),

    %

    YieldStrength

    (0.2% offset),1000 psi

    Elongationin 2 in.,

    %

    Hardness,Brinell orRockwell

    TensileStrength,1000 psi

    Form andCondition

    COP PER AND COP PER ALL 0 YS (continued)

    M BronzeCastings-ASTM 8143 Alloy 28 70

    Cu-balSn- 8.5Zn- 4

    As Cast 52 48

    Leaded Tin Bronze(83-7-7-3)Castings-ASTM 8144 Alloy 38

    Cu-83Zn- 7Pb- 7Sn- 3

    As Cast 34 18 60

    Nickel-Tin Bronze Type ACastings-ASTM 8292

    85Cu-balNi - 5Sn- 5Zn- 2

    As Cast 20 50 40

    HeatTreated 1400F (W.Q.)and 600 F 10 18055 85

    Nickel- Tin Bronze Type BCastings-ASTM 8 292 30

    Cu-balNi - 5Sn- 5Pb- 1Zn- 2

    As Cast 20

    30

    45 80

    120Tempered (575 F) 60 8

    Copper-NickelCastings-ASTM 8369 Alloy A

    Cu-balNi -10Mn-- 0.6Fe - 1.3Si - 0.3Cb- 0.7

    As Cast 25 45 30 90

    Copper-NickelCastings-ASTM 8369 Alloy 8

    Cu-balNi -30Mn- 0.75Fe - 0.8Si - 0.4Cb- 0.7

    As Cast

    Nickel SilverCastings-ASTM 8149 No. lOA

    Cu-55Zn-balNi -12.5Pb-l0Sn- 2

    As Cast 18 35 15 55

    Nickel SilverCastings-ASTM 8149 No. lIA

    Cu-65Zn-balNi -20Pb- 4Sn- 4

    As Cast 26 47 22 85

    Nickel SilverCastings-ASTM 8149 No. 118

    Cu-55Zn-balNi -25Pb- 2Sn- 5

    As Cast 50 18 58

    WHITE METALS AND ALLOYS

    AntimonyIngots-ASTM 8237

    Sb-99.8 min 42Cast (I ngot) 1.56

    Bismuth-Lead Alloy Bi -55.5Pb-44.5

    Cast 65 106.4

    Bismuth-Tin Alloy 8.08i -58Sn-42

    200 22Cast

    a=O.5% Extension

    10

    b=Depends on Cooling Rate

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F). (32 to 212 F). Resistivity. Modulus ModulusDensity. Melting Point. (32 to 212 F). in 10- Btu/sq It (68 F) ohms of Elasticity. of Elasticity.Ib/cu in. Specific Gravity F Btu/lb/"F in./inpF /hr /"F fin. /cir mil It in 10 psi x 10 psi Material

    COPPER AND COPPER ALLOYS (continued)M Bronze

    0.318 8.80 1832 102 14

    leaded Tin Bronze0.322 8.93 1800 10 14.5

    0.320 8.86 1950 11 15 Nickel- Tin BronzeType A

    Nickel Tin Bronze0.320 8.86 1925 10 13 Type B

    14

    CopperNickel

    0.323 8.94 2100 9.52 17

    Copper-Nickel

    0.323 8.94 2260 9.42 18

    Nickel Silver

    0.320 8.86 1830 0.l2 10.0 120 204 19

    Nickel Silver

    0.321 8.89 2090 150 19

    Nicke I Silver

    0.320 8.86 1910 19

    WHITE METALS AND ALLOYS0.249 6.62 1166 0.092 5.5 131 234 11.3 2.8 Antimony

    0.380 10.5 255 0.03* 11.6 Bismuth-leadAlloy

    0.315 8.72 281 0.045* 8.3* Bismuth-TinAlloy

    *= Estimated 2=68 to 572 F

    11

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness.(essential elements). Form and (0.2% offset). Strength. in 2 in. Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    WHITE METALS AND ALLOYS (continued)Bismuth-Lead- Tin-Cadmium Alloy Bi -50

    Pb-26.7 Cast 5.99 200 9Sn-13.3Cd-l0

    Bismuth-Lead-Indium-Cadmium- Bi -44.7Tin Alloy Pb-22.6

    In -19.1 Cast 5.4 1.5 12Cd - 5.3Sn - 8.3

    Lead Pb-99.9 min Rolled 1.9 2.5 50 5Pig Form-ASTM B 29

    Antimonial Lead Pb-90 Cast 6.8 24 13Die Castings-ASTM B 102 Sb-lO

    Rolled 4.1 47 9

    Tellurium Lead Pb-99.85Te- 0.04 Rolled 2.2 3 45 6Cu- 0.06

    5050 Solder Sn-50 Cast 6.8 50 14ASTM B 32 Grade 50A Pb-50

    6040 Solder Sn-60 Cast 7.1 45 15Pb-40

    Tin Sn -99.98 min Cast 2.1 70 3.9ASTM B 339 Grade AA

    , Zinc Zn-bal Hot Rolled (Longitudinal) 19.5 65 38Rolled-ASTM B 69 Pb- 0.08

    Cold Rolled 21 50

    ZILLOY* 15 Zn-bal Hot Rolled (Longitudinal) 29 20 61Mg- 0.01Cu- 1.00 Cold Rolled 36 25 80

    Zinc-Aluminum Alloy Zn-balDie Castings-ASTM B 86 AI- 4 Die Cast 41 10 82

    Mg- 0.04

    Zinc-Aluminum-Copper Alloy Zn-balASTM B 25 AI- 3.9 Die Cast 47.6 7 91

    Mg- 0.05Cu- 1.00

    C.D.C. Manganese Alloy 772 Mn-72Cu-18 Rolled 95 115 6.5Ni -10

    ALUMINUM AND ALLOYSAluminum Alloy 1100 Sheet Annealed 5 13 35 23

    Sheet & Plate-ASTM B 209 AI-99.0 minCold Rolled 22 24 5 44

    Aluminum Alloy 2017 AI-bal Bar Annealed 10 26 22 45Bar, Rod & Wire-ASTM B 211 Cu- 4

    Mn- 0.5 Heat Treated 40 62 22 105Mg- 0.5

    'See page 62 for list of trademarks

    12

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./inpF /hr rF fin. /cir mil ft in 106 psi x 106 psi Material

    WHITE METALS AND ALLOYS (continued)

    Bismuth-Lead-0.339 9.38 158 0.040** 12.2** Tin-Cadmium

    Alloy

    Bismuth-Lead-Indium-

    0.320 8.85 117 0.035** 13.8*' Cadmium-Tin Alloy

    0.410 11.35 621 0.030 16.4 240 124 2 Lead

    0.393 10.88 545 0.032 15.1 200 152 3 Antimonial Lead

    Tellurium Lead0.410 11.35 621 0.030 16.4 240 124 2

    0.321 8.89 421 0.051 13.1 310 93 50-50 Solder

    0.306 8.50 374 0.055 12.2 330 90 6040 Solder

    0.263 7.29 449 0.095 12.8 428 66 6 Tin

    0.258 7.14 786 0.094 18 746 35.5 Zinc

    0.259 7.18 792 0.096 19.3 726 38 ZILLOY*15

    Zinc-Aluminum0.24 6.6 728 0.10 15.2 784 38.2 Alloy

    Zinc-Aluminum-0.240 .6.70 727 0.10 15.2 755 39.2 Copper Alloy

    C. D. C. Manganese0.26 7.21 0.12 15.31 58 1050 18 Alloy

    772

    ALUMINUM AND ALLOYS

    0.098 2.71 1215 0.23 13.11 1540" 17 10.0 3.75 Aluminum Alloy1100

    1510" 18 10.0 3.75

    0.101 2.79 1185 0.23 12.71 11905 23 10.5 4.0 Aluminum Alloy2017

    8405 35 10.5 4.0

    **Estimated 1=68 to 212 F "=at77 F

    13

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    ALUMINUM AND ALLOYS (continued)Aluminum Alloy Alclad 2024 Core: 2024

    Sheet & Plate-ASTM B 209 AI-balCu- 4.5 Sheet Annealed 11 26 20Mn- 0.6Mg- 1.5 Heat Treated 42 64 19Cladding:AI-99.3 min

    Aluminum Alloy 3003 AI-bal Sheet Annealed 6 16 30 28Sheet & Plate-ASTM B 209 Mn- 1.2

    Cold Rolled 27 29 4 55

    Aluminum Alloy 5052 AI-bal Sheet Annealed 13 28 25 47Sheet & Plate-ASTM B 209 Mg- 2.5

    Cr - 0.25 Cold Rolled 37 42 7 77

    Aluminum Alloy 6061 AI-balSheet & Plate-ASTM B 209 Si - 0.6 Sheet Annealed 8 18 25 30

    Cu- 0.25Mg- 1.0 Heat Treated 40 45 12 95Cr - 0.25

    Aluminum Alloy 7075 AI-balBar, Rod, Wire & Shapes- Zn- 5.6 Bar Annealed 15 33 16 60ASTM B 221 Cu - 1.6

    Mg- 2.5 Heat Treated 73 83 11 150Cr - 0.3

    Cast Aluminum Alloy 13 AI-bal Die CastingCastings-ASTM B 85 Grade S12A Si -12.0 21 43 2.5

    As Cast

    Cast Aluminum Alloy 43 AI-bal Permanent Mold CastingCastings-ASTM B 108 Grade S5B Si - 5.0 9 23 10 45

    As Cast

    Cast Aluminum Alloy 380 AI-bal Die CastingCastings-ASTM B 85 Grade SC84A Cu- 3.5 24 48 3

    Si - 9.0 As Cast

    Cast Aluminum Alloy 195 AI-bal Sand CastingCastings-ASTM B 26 Grade C4A Cu- 4.5 24 36

    Si - 0.8 Heat Treated

    Cast Aluminum Alloy 214 AI-bal Sand CastingCastings-ASTM B 26 Grade G4A Mg- 3.8 12 25 9 50

    As Cast

    Cast Aluminum Alloy 220 AI-bal Sand Casti ngCastings-ASTM B 26 Grade GlOA Mg-lO.O 26 48 16 75

    Solution Heat Treated

    Cast Aluminum Alloy A132 AI-balCastings-ASTM B 108 SN122A Si -12.0 Permanent Mold Casting

    Mg- 1.2 Heat Treated 43 47 0.5 125Ni - 2.5 Plus 340 FCu - 0.8

    Cast Aluminum Alloy 142 AI-balCastings-ASTM B 26 CN42A Mg- 1.5 Sand Casting 30 32 0.5 85

    Ni- 2.0 Heat Treated Plus 650 FCu- 4.0

    14

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile TorsionalSpecific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu /sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb/"F in./in.;oF /hr/"F fin. /cir mil ft in 106 psi x 106 psi Material

    ALUMINUM AND ALLOYS (continued)Aluminum Alloy

    Alclad0.100 2.77 1180 0.23 12.61 13405 21 10.6 3.75 2024

    8405 35 10.6 4.0

    0.099 2.73 1210 0.23 12.91 13405 21 10.0 3.75 Aluminum Alloy3003

    10705 26 10.0 . 3.75

    0.097 2.68 1200 0.23 13.21 9605 30 10.2 3.75 Aluminum Alloy5052

    9605 30 10.2 3.75

    Aluminum Alloy0.098 2.70 1205 0.23 13.01 11905 23 10.0 3.75 6061

    10705 26 10.0 3.75

    Aluminum Alloy0.101 2.80 1175 0.23 12.91 10.4 3.9 7075

    8405 35 10.4 3.9

    Cast Aluminum0.096 2.65 1080 0.23 11.51 8705 34 10.3 3.85 Alloy

    13

    Cast Aluminum0.097 2.69 1170 0,23 12.31 9905 28 10.3 3.85 Alloy

    43

    Cast Aluminum0.098 2.72 1100 0.23 11.61 6705 45 10.3 3.85 Alloy

    380

    Cast Aluminum0.102 2.81 1190 0.23 12.71 9605 30 10.0 3.75 Alloy

    195

    Cast Aluminum0.096 2.65 1185 0.23 13.41 9645 30 10.3 3.85 Alloy

    214

    Cast Aluminum0.093 2.57 1120 0.23 13.71 6105 50 9.5 3.55 Alloy

    220

    Cast AluminumAlloy

    0.098 2.72 1050 0.23 11.01 8105 36 10.6 4.35 A 132

    Cast Aluminum0.102 2.81 1175 0.23 12.61 9305 31 10.3 3.85 Alloy

    142

    1=68 to 212 F 5=at 77 F

    15

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness.(essential elements). Form and (0.2% offset). Strength. in 2 in., Brinell or

    Material % Condition 1000psi 1000psi % Rockwell

    MAGNESIUM ALLOYS

    Magnesium Alloy AZ318 Mg-bal Sheet Annealed 22 37 21 56Plate & Sheet-ASTM B 90 AI- 3.0

    Zn - 1.0 Hard Sheet 32 42 15 73Mn- 0.2 min

    Magnesium Alloy AZ80A Mg-bal As Forged 33 48 11 69Forgings-ASTM B 91 AI- 8.5

    Zn- 0.5 Forged and Aged 36 50 6 72Mn- 0.15 min

    Magnesium Alloys AZ91A & AZ91B Mg-balCastings-ASTM B 94 AI- 9.0 Die Cast 22 33 3 63

    Zn - 0.7Mn- 0.2 min

    Cast Magnesium Alloy AZ91C Mg-bal As Cast 14 24 2.5 60Castings-ASTM B 199 (Permanent), AI - 8.7ASTM B 80 (Sand) Zn - 0.7 Solution Treated and Aged 19 40 5 70

    Mn- 0.2 min

    Magnesium Alloy AZ92A Mg-bal As Cast 14 25 2 65Castings-ASTM B 199 (Permanent). AI- 9ASTM B 80 (Sand) Zn- 2 Solution Treated 14 40 10 63

    Mn- 0.10 minSolution Treated and Aged 22 40 3 81

    Magnesium Alloy EZ 33A Mg-balCastings-ASTM B 199 (Permanent) Zn - 2.6 Aged Castings 16 23 3 50

    Zr - 0.7Other elements-3

    Magnesium Alloy HK31A Mg-bal Strain Hardened Partially-Plate & Sheet-ASTM B 90 Th- 3.25 Sheet Annealed 29 37 8 68Castings-ASTM B 199 (Permanent) Zr - 0.7

    Castings-Heat Treated 15 32 8 RB66

    Magnesium Alloy HZ 32A Mg-balCastings-ASTM B 80 (Sand) Th- 3.25 Solution Treated and

    Zn - 2.1 Aged Castings 13 27 4 55Zr - 0.7

    Magnesium Alloy ZK60A Mg-bal As Extruded 38 49 14 75Extrusions-ASTM B 107 Zn - 5.5Forgings-ASTM B 91 Zr - 0.55 Aged 44 53 11 82

    TITANIUM ALLOYS

    Titanium Ti-3SA Ti -balForgings-ASTM B 381 C - 0.08 maxSheet. Strip & Plate-ASTM B 265 Fe - 0.12 max Sheet Annealed 30 40 30 135Pipe-ASTM B 337 Nz - 0.05 maxTubes-ASTM B 338 Hz - 0.Dl5 maxBars-ASTM B 348

    Titanium Ti-SOA Ti -balForgings-ASTM B381 C - 0.08 maxSheet. Strip & Plate-ASTM B 265 Fe - 0.20 max Sheet Annealed 45 55 25 215Pipe-ASTM B 337 Nz - 0.05 maxTubes-ASTM B338 Hz - 0.Gl5 maxBars-ASTM B 348

    16

  • Typical Physical Properties

    Thermal Expan- Therinalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-' Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./in.;oF /hr rF fin. /cir mil ft in 10' psi x 10' psi Material

    MAGNESIUM ALLOYS0.064 1.77 1170 0.245 14.51 6576 55 6.5 2.4 Magnesium Alloy

    AZ31B

    0.065 1.80 1130 0.25 14.51 5222 87 6.5 2.4 Magnesium AlloyAZSOA

    0.065 1.80 1105 0.25 14.51 4932 102 6.5 2.4 Magnesium AlloysAZ91AAZ91B

    0.065 1.81 1105 0.25 14.51 4932 90 6.5 2.4 Cast MagnesiumAlloy

    91 AZ 91C

    0.066 1.82 1100 0.25 14.01 4932 84 6.5 2.4 Magnesium AlloyAZ92A

    99

    84

    Magnesium Alloy0.066 1.83 1189 0.25 14.51 6966 42 6.5 2.4 EZ 33A

    Magnesi urn Alloy0.065 1.79 1204 0.24 7846 37 6.5 2.4 HK31A

    6396 46 6.5 2.4

    Magnesium AlloyHZ 32A

    0.066 1.83 1198 0.23 14.84 7556 39 6.5 2.4

    0.066 1.83 1175 0.24 14.51 8156 36 6.5 2.4 Magnesium AlloyZK 60A

    8456

    TITANIUM ALLOYSTitanium

    Ti-35A0.163 4.50 3063 0.l24 4.8 1083 336 14.9 6.5

    TitaniumTi-50A

    0.163 4.50 3100 0.125 4.8 1143 336 14.9 6.5

    1=6810212 F 2=6810575 F 3=a168 F '_6810392 F 6 Near RoomTemperalure

    17

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinel! or

    Material % Condition 1000 psi 1000 psi % Rockwell

    TITANIUM ALLOYS (continued)

    Titanium Ti-75A Ti -balSheet, Strip & Plate-ASTM B 265 C - 0.08 maxPipe-ASTM B 337 Fe- 0.30 max Sheet Annealed 75 85 18 245Tube-ASTM B 338 N,- 0.05 maxBar-ASTM B 348 H, - 0.D15 max

    Ti-O.2 Pd Alloy Ti -balPipe-ASTM B 337 Pd- 0.2Tube-ASTM B 338 C - 0.08 max Sheet Annealed 45 55 25 215

    Fe- 0.20 maxN2- 0.05 maxH, - 0.015 max

    TI-5 AI-2.5 Sn Alloy Ti -balSheet, Strip & Plate-ASTM B 265 AI- 5Bar-ASTM B 348 Sn- 2.5Forgings-ASTM B 381 C - 0.08 max Annealed 125 135 13 Rc39

    Fe - 0.05 maxN,- 0.05 maxH, - 0.0175 max

    TI-8 AI-l Mo-l V Alloy Ti -balPlate, Sheet & Strip-AMS 4915 AI- 8

    Mo-1V -1 Sheet Annealed 130 140 13 Rc39C - 0.08 maxN2- 0.05 maxH2 - 0.D15 max

    Ti-6 AI-2 Sn-4 Zr-2 Mo Alloy Ti -balAI- 6Sn- 2Zr - 4Mo- 2 Bar Annealed 130 140 15 Rc39C - 0.4 maxFe - 0.15 maxN,- 0.04 maxH, - 0.015 max

    Ti-6 AI-6 V-2 Sn Alloy Ti -balForgings-ASTM B 381 AI- 5.5

    V - 5.5Sn- 2Cu- 0.7 Sheet Annealed 155 165 12 Rc41Fe - 0.7C - 0.05 maxN,- 0.04 maxH, - 0.015 max

    Ti-6 AI-4 V Alloy Ti -balSheet, Strip, Plate-ASTM B265 AI- 6.5Bar-ASTM B 348 V - 4 Sheet Annealed 130 140 13 Rc39Forgings-ASTM B 381 C - 0.08 max

    Fe - 0.25 max Heat Treated 165 175 12N2- 0.05 maxH, - 0.D15 max

    Ti-13 V-II Cr-3 AI Alloy Ti -balPlate, Sheet & Strip-AMS 4917 V -13.5

    Cr -10.5 Sheet Annealed 130 135 13 Rc37AI- 3C - 0.05 max Heat Treated 170 180 6N,- 0.08 maxH, - 0.025 max

    18

  • Typical Physical PropertiesThermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb/"F in./inpF /hr /"F fin. /cir mil ft in 106 psi x 106 psi Material

    TITANIUM ALLOYS (continued)

    TitaniumTi-75A

    0.164 4.53 3038 0.129 4.8 1183 360 15.1 6.5

    Ti-O.2 Pd Alloy

    0.163 4.50 3100 0.125 4.8 1143 340 14.9 6.5

    Ti-5 AI-2.5 SnAlloy

    0.162 4.47 3002 0.125 5.2 1092 16 7.0

    Ti-8 AI-I Mo-I VAlloy

    0.158 4.36 4.7 1192 17.5

    Ti-6 AI-2 Sn-4Zr-2 MoAlloy

    0.164 4.53 3000 16.5

    Ti-6 AI-6 V-2 SnAlloy

    0.164 4.53 3100 0.155 5.0 503 942 16.5

    Ti-6 AI-4 VAlloy

    0.160 4.42 3000 0.135 4.9 503 1026 16.5 6.1

    0.175 4.83 0.120 483 918 15 6.2

    Ti-13 V-II Cr-3 AIAlloy

    4=68 to 392 F

    19

  • Properties OF SOME METALS AND ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness.(essential elements). Form and (0.2% offset). Strength. in 2 in.. Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    RESISTANCE HEATING ALLOYS

    80 Ni-20 Cr Alloy Ni -80 Annealed 60 100 30 RB88ASTM B 344 Cr-20

    60 Ni-15 Cr-bal Fe Alloy Ni -60ASTM-B344 Cr -15 Annealed 50 105 30 200

    Fe -bal

    35 Ni-20 Cr-bal Fe Alloy Fe-balASTM-B344 Ni -35 Annealed 55 102 30 RB83

    Cr-20

    Ni-Cr AlloyA Ni -balCr-20 Annealed 65 140 35AI- 3Fe- 3

    Fe-Cr-AI AlloyB Fe-balCr-23 Annealed 80 100 25 215AI- 5Co -May be present

    MAGNETIC ALLOYS

    79 Ni-4 Mo Alloy Ni -79(Magnetically Soft) Mo- 4 Magnetic Annealed 22 79 64 RB62

    Fe -bal

    Mu Metal Fe-bal Strip Mill Annealed 38 90 35(Magnetically Soft) Ni -77

    Cu- 5 Hydrogen Annealed 18 64 27 RB60Cr - 1.5

    49 Ni-bal Fe Alloy Fe-bal Strip Mill Annealed 40 80 33(Magnetically Soft) Ni -49

    Hydrogen Annealed

    Alnico II Fe -bal(Permanent Magnet Alloy) AI-lO Cast Annealed 3 Rc45

    Ni -18Co-13 Sintered 65 Rc43Cu- 6

    Alnico III Fe-bal(Permanent Magnet Alloy) AI-12 Cast Annealed 12 Rc45

    Ni -26Cu- 3

    Alnico IV Fe -bal Cast Annealed 9.1 Rc45(Permanent Magnet Alloy) AI-12

    Ni -28 Sintered 60 Rc42Co- 5

    Alnico V** Fe-bal(Permanent Magnet Alloy) AI- 8 Cast Cooled in Magnetic Field 5.4 Rc50

    Ni -15Co-24 Sintered 50 Rc44Cu- 3

    Alnico VI** Fe -bal(Permanent Magnet Alloy) AI- 8 Cast Cooled in Magnetic Field 23 Rc50

    Ni -16Co-24 Sintered Rc44Cu- 3Ti - 1.25

    B Marketed, with minor chemical variations,under the following trademarks:KANTHAL * 200 ALLOY* ALCHROME*

    *See page 62 for list of trademarks **Properties Depend on Cooling RateA Developed for applications requiring a neg-ligible temperature coefficient of resistancein the temperature range of -60 to 480 F.Marketed. with minor chemical variations.under the following trademarks:KARMA* EVANOHM* NIKROTHAL*

    20

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb;oF in./in.;oF /hr;oF fin. /cir mil It in 106 psi x 106 psi Material

    RESISTANCE HEATING ALLOYS

    0.304 8.41 2550 0.104 7.3 10410 650 31 80 Ni-20 Cr9.615 Alloy

    60 Ni-15 Cr-0.298 8.25 2460 0.112 7.6 9310 675 29 bal Fe Alloy

    9.415

    35 Ni-20 Cr-0.287 7.95 2515 0.098 8.816 14810 610 27 bal Fe Alloy

    Ni-Cr AlloyA0.293 8.11 2550 0.104 7.4 88 800

    Fe-Cr-AI0.262 7.25 2750 9.316 812 AlloyD

    MAGNETIC ALLOYS

    79 Ni-4 Mo Alloy0.315 8.72 2600 0.12 7.0 232 350 33.3 6.6

    30 Mu Metal

    8.5 7.01 337 25

    49 Ni-bal Fe Alloy

    8.2 4.71 270

    Alnico 0.256 6.92 3905

    0.243 6.92 4085

    Alnico III0.249 7.22 3605

    0.253 7.32 4505 Alnico IV

    0.232 7.32 4085

    Alnico V**0.265 6.32 2825

    0.241 6.32 3005

    Alnico VI**0.268 6.32 3005

    0.241 6.32 3185

    1=68 to 212 F 2=68 to 572 F 5=at 77 F 15=68 to 1832 F 16=68 to 937 F

    21

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    MAGNETIC ALLOYS (continued) ;-

    Alnico VII** Fe-bal(Permanent Magnet Alloy) AI- 8.5

    Ni -18 Cast Cooled in Magnetic Field Re60Co-24Cu- 3.25Ti - 5

    Alnico VIII** Fe -bal(Permanent Magnet Alloy) AI- 7

    Ni -15 Cast Cooled in Magnetic Field Re57Co-35Cu- 4Ti - 5

    eunico Cu-50 Strip Cold Rolled(Permanent Magnet Alloy) Ni -21 Heat Treated 100 RB95

    Co-29

    Cunife Cu-60 Strip Cold Rolled(Permanent Magnet Alloy) Ni -20 Heat Treated 100 RB73

    Fe-20

    CONTROLLED EXPANSION ALLOYS

    INVAR* Ni -36 Annealed 40 71 43 132Fe-bal

    42 Ni-Iron Alloy Ni -42 35 68 45 138ASTM F30 Fe-bal

    49 Ni-Iron Alloy Ni -49 Annealed 33 77 45 144ASTM F30 Fe-bal

    lron- Nickel Temperature Ni -29.5Compensating Alloys Fe -bal

    Ni -31 Annealed 65 125Fe -balNi -32.5Fe -bal

    Ni-fe-Co Alloye Fe -balNi -29 Annealed 35 85 40Co-17

    NISPANC* Ni( +Co)-42.10 Annealed 35 90 40 125Mn- 0.40Fe -48.45 Aged 115 180 18 305Cr - 5.35Ti - 2.40 Cold Rolled 50% 130 135 6 270AI - 0.65

    Cold Rolled and Aged 1250 F 180 200 7 395

    ISOElASTlC* Ni( +Co)-36.85Fe -54.25 Annealed 35 85 30 135Mn- 0.55Cr - 7.10 Cold Worked 135 155 10 305Mo- 0.45

    C Also available, with minor chemical varia- * See page 62 for list of trademarks ** Properties Depend on Cooling Ratetions, under the following trademarks:THERLO* RODAR* KOYAR*

    22

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lb/"F

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in./in./"F

    ThermalConductivity(32 to 212 F),

    Btu/sq It/hr /"F fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    MAG N ETI C ALLOY S (continued)

    Alnico VII**

    0.259 6.12 3485

    Alnico VIII**

    0.265 3005

    Cunico0.300 7.82 1445

    Cunife0.311 7.82 1085

    CONTROLLED EXPANSION ALLOYS

    0.293 8.11 2600 0.12 0.8 72.6 494 21 8.1 INVAR*

    0.294 8.13 2600 0.12 2.9 106 405 22 8.5 42 Ni-Iron Alloy

    0.297 8.23 2600 0.12 4.9 124 270 24 9.3 49 Ni-Iron Alloy

    Iron- NickelTemperature

    0.295 to 0.292 8.2 to 8.12 0.12 6.0 to 3.0 80 480 22 CompensatingAlloys

    Ni-fe-Co Alloy

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness.(essential elements). Form and (0.2% offset). Strength. in 2 in. Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    NICKEL AND ALLOYS

    Nickel 211 Ni -95.0ASTM F290 Mn- 4.75 Annealed 35 75 40 140

    C - 0.10

    Nickel Ni -95.6(Cast) Cu- 0.5

    Fe - 0.5 As Cast 25a 57 22 110Mn- 0.8Si - 1.5C - 0.8

    Nickel 200 Ni -99.5Plate. Sheet. Strip-ASTM B 162 Mn- 0.25 Rod Hot Rolled Annealed 21.5 67 47 100Bar-ASTM B 160 Fe - 0.15Pipe & Tube-ASTM B 161 & B 163 C - 0.06

    Nickel 201 Ni -99.5Plate. Sheet. Strip-ASTM B 162 Mn- 0.20 Rod Hot Rolled Annealed 18 55 55 90Bar-ASTM B 160 Fe - 0.15Pipe & Tube-ASTM B161 & B 163 C - 0.01

    Nickel 205 Ni -99.5Mn- 0.20Fe - 0.10 Rod Hot Rolled Annealed 21 67 47 100Ti - 0.02Mg- 0.04C - 0.06

    Nickel 270 Ni -99.98 Strip Annealed 13 50 45 RB30Electronic Sleeves-ASTM F239

    PERMANICKEL* Alloy 300 Ni -balMn- 0.25 Rod Annealed 45 121 41 160Ti - 0.50Mg- 0.35 Annealed and Aged 140 176 16 325C - 0.25

    DURANICKEL* Alloy 301 Ni -balAI- 4.5Si - 0.55Ti - 0.5 Hot Rolled and Aged 132 185 28 330Mn- 0.25Fe - 0.15C - 0.15

    Nickel Beryllium 440 Ni -bal Strip Annealed 45 105 40 RB70(Wrought) Be- 1.95

    Ti - 0.5 Annealed and Aged 150 215 15 Re47

    Nickel Beryllium M220C Ni -bal Casting Annealed 60 110 10 Re28(Cast) Be- 2.15

    C - 0.4 max Annealed and Aged 180 190 2 Re51

    Nickel Beryllium CR-l Ni -bal As Cast 70 125 2 285(Cast) Be- 2.7

    Cr - 0.7 Annealed and Aged at 950 F 180 195 0 328C - 0.1

    WAUKESHA METAl* No.23 Ni -78(Non-Galling Alloy) Pb- 4

    Sn- 8 As Cast 55 75 11 160Zn - 7.5Mn- 2

    * See page 62 for list of trademarks

    24

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb/"F in./inpF jhr/"F fin. /cir mil It in 106 psi x 106 psi Material

    NICKEL AND AllOYSNickel

    0.315 8.73 2600 0.11 7.417 3063 102 30 11 211

    Nickel(Cast)

    0.301 8.34 2550 0.13 8.85 410 125 2l.5

    Nickel0.321 8.89 2635 0.11 7.417 5203 57 30 11 200

    Nickel0.321 8.89 2635 0.11 7.2 5503 46 30 11 201

    Nickel205

    0.321 8.89 2635 0.11 7.417 5203 57 30 11

    0.321 8.89 2650 0.11 7.417 595 45 30 Nickel270

    PERMANICKEL*0.316 8.75 2620 0.106 6.817 4003 95 30 11 Alloy

    300

    DURANICKEL*Alloy301

    0.298 8.75 2620 0.104 7.2 1653 255 30 11

    0.318 8.84 8.01S 2203 143 28.5 Nickel Beryllium440

    0.29 8.10 2310 7.74 2153 27 Nickel BerylliumM220C

    0.287 7.95 2310 345 to l72 25 to 28 Nickel BerylliumCR-1

    WAUKESHAMETAL

    7.4831 22 No.23

    3=8177 F 4=6810392 F 17=710200 F IS=al 500 F 31 32 10500 F

    25

  • Properties OF SOME METALS AND ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    NICKEL AND ALLOYS (continued)

    WAUKESHA METAL* No. 88 Ni -bal(Non-Galling Alloy) Fe- 5

    Cr -12.5Mo- 3 As Cast 40 50 10 150Bi - 4Sn- 4Mn- 0.8

    MONEL* NICKEL-COPPER ALLOYS

    MONEl* Alloy 400 Ni -balRod & Bar-ASTM B 164 Cu-31.5Plate, Sheet, Strip-ASTM B 127 Fe - 1.35 Rod Hot Rolled Annealed 30 79 48 125Tube-ASTM B 165 Mn- 0.90

    Si - 0.15C - 0.12

    MONEl* Alloy 401 Ni -44.5Cu-53.0Co- 0.50 Rod Hot Rolled Annealed 25 63 48 100Mn- 1.70Fe - 0.20

    MONEl* Alloy 404 Ni -55Cu-44 Rod Hot Rolled 31 69 45 RB67Mn- 0.01Fe - 0.05 Strip Annealed 22 64 43 RB54C - 0.06

    MONEl* Alloy R-405 Ni -66.0Rod-ASTM B 164 Class B Cu -31.5 Hot Rolled 45 85 35 145

    Fe - 1.35Mn- 0.90 Cold Drawn 75 100 25 200Si - 0.15C - 0.18

    MONEL' Alloy K500 Ni -balBar & Forgings-AMS 4676 Cu-29.5

    AI- 2.8 Rod As Hot Rolled 49 97 44 155Ti - 0.5Fe - 1 Hot Rolled Aged 111 160 23.5 300Mn- 0.6C - 0.15Si - 0.15

    MONEl* Alloy 410 Ni -66(Cast) Cu-30.5

    Fe - 1.0 As Cast 35 75 40 150Mn- 0.8 I.;Si - 1.6

    MONEL* Alloy 505 Ni -64(Cast) Cu-29 Casting Annealed 75 115 10 225

    Fe - 2Mn-- 0.8 As Cast or Annealed and Aged 110 135 2 340Si - 4.0

    * See page 62 for trademarks

    26

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbj"F

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in./inpF

    ThermalConductivity(32 to 212 F),

    Btu /sq It/hrj"F fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    N ic KELAN 0 ALL 0 YS (continued)WAUKESHA

    METAL*No.88

    8.031 26

    MONEL* NICKEL-COPPER ALLOYS

    0.319 8.84 2460 0.102 7.711 1513 307 26 9.5

    MONEL*Alloy400

    MONEL*Alloy

    0.321 8.88 7.611 310 401

    MONEL*0.321 8.88 0.099 7.411 300 25 9.4 Alloy

    404

    MONEL*0.319 8.84 2460 0.102 7)11 1513 307 26 9.5 Alloy

    R405

    0.306 8.46 2460 0.100 7.611 121314510

    370 26 9.5

    MONEL*AlloyK500

    MONEL*Alloy

    0.312 8.63 2450 0.13 9.232 1861 320 23 410

    MONEL~0.302 8.36 2350 0.13 8.932 1361 380 24 Alloy

    505

    1=68 to 212 F 3=at 68 F 10=at 212 F 17=70 to 200 F 31=32 to 500 F 32= 70 to 1100 F

    27

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    INCOlOY* NICKEL-IRON-CHROMIUM ALLOYS

    INCOlOY* Alloy 800 Ni -32Plate, Sheet, Strip-ASTM B 409 Cr -20.5Rod & Bar-ASTM B408 Fe-46 Rod Hot Rolled Annealed 42 87 44 150Pipe & Tube-ASTM B 163 & B 407 C - 0.04

    Ti - 0.4AI- 0.4

    INCOlOY* Alloy 802 Ni -32 Annealed 45 95 40 185Cr -20.5Fe-46 Cold Drawn 155 10 255C - 0.35

    I N CO lO y* Alloy 825 Ni -41.8Plate, Sheet, Strip-ASTM B 424 Cr -21.5Rod & Bar-ASTM B425 Fe-30Pipe-ASTM B 423 Cu- 1.8 Rod Annealed 35 91 50

    Mo- 3Ti - 0.9AI - 0.15C - 0.03

    INCONEl* NICKEL-CHROMIUM-IRON ALLOYS

    INCONEL* Alloy 600 Ni -balPlate, Sheet, Strip-ASTM B 168 Cr -15.8Rod & Bar-ASTM B 166 Fe - 7.2Pipe & Tube-ASTM B 163 & B 167 Mn- 0.2 Rod Hot Rolled Annealed 36 90 47 150

    Si - 0.2C - 0.04Cu- 0.10

    INCONEL* Alloy 625 Ni -balCr -18.6Fe- 3 Rod Hot Rolled Annealed 86 142 42 280Cb- 4Mo- 9C - 0.05

    INCONEl* Alloy 718 Ni -balPlate, Sheet, Strip-AMS 5597 Cr -18.6Bar-AMS 5664 Fe -18.5 Rod Hot Rolled,

    AI- 0.4 Annealed and Aged 174 211 23Ti - 0.9Cb- 5Mo- 3.1C - 0.04

    INCONEL* Alloy X-750 Ni -balBar-ASTM A 461 Grade 688 Cr -15.0 Rod Hot Rolled,

    Fe - 6.75 1625 F and Aged 138 188 18AI- 0.8Ti - 2.5 Sheet Annealed and Aged 120 180 24Cb- 0.85Mn- 0.7C - 0.04

    INCONEL* Alloy 751 Ni -balCr -15Fe - 6.75 Annealed 75 125 50 176AI - 1.2Ti - 2.5 Annealed and Aged no 175 20 337Cb- 1Mn- 0.7C - 0.04

    * See page 62 for list of trademarks

    28

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in./inpF

    ThermalConductivity(32 to 212 F),

    Btu/sq ft/hr rF fin.

    ElectricalResistivity,(68 F) ohms/cir mil ft

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    INCOLOY* NICKEL.IRONCHROMIUM ALLOYS

    0.290 8.01 2525 0.120 7.917 803 595 28 11

    INCOlOY*Alloy800

    0.294 8.14 28.5 INCOlOY*Alloy802

    INCOlOY*Alloy825

    0.294 8.14 2550 7.817 773 678 28

    INCONEL* NICKEL.CHROMIUMIRON ALLOYSINCONEL*

    Alloy600

    0.304 8.43 2600 0.106 7.417 1033 620 31 11

    0.305 8.45 0.098 7.117 683 776 29.8 11.4INCONEL*

    Alloy625

    INCONEL*Alloy718

    0.296 8.19 7.217 783 731 29 11.2

    0.298 8.25 2600 0.103 7.017 833 731 31 11

    INCONEL*AlloyX-750

    0.298 8.25 2600 743 30 11

    INCONEL*Alloy751

    17=70 to 200 F

    29

  • Properties OF SOME METALS AND ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness.(essential elements). Form and (0.2% offset). Strength. in 2 in.. Brineli or

    Material % Condition 1000 psi 1000 psi % Rockwell

    NIMONIC* NICKEL-CHROMIUM ALLOYSNIMONIC' Alloy 75 Ni -77.4

    Cr -20.5AI - 0.15 Bar Hot Rolled Annealed 51 116 44 RB87Ti - 0.35Fe- 0.5C - 0.10

    NIMONIC' Alloy BOA Ni -74.5Cr -20.5AI- 1.25 1975 F. Air Cool plus 1300 F 90 154 39 Rc34Ti - 2.4Fe - 0.5C - 0.05

    NIMONIC' Alloy 90 Ni -57Cr -20.5Co-17AI- 1.6 1975 F. Air Cool plus 1300 F 116 179 33 Rc38Ti - 2.6Fe - 0.5C - 0.05

    NIMONIC' Alloy 115 Ni -balCr-15Co-15 2175 F. Air Cool plus 2010 F 125 180 27 Rc37Mo- 3.5Ti - 4AI- 5

    HASTELLOY* ALLOYSHASTELLOY' Alloy B Ni -bal Sheet Annealed 57 121 63 RB92

    Plate & Sheet-ASTM B 333 Mo-28Rod-ASTM B 335 Fe- 5 Sand-Cast Annealed 50 90 10 RB93Castings-ASTM A 494 V - 0.3

    HASTELLOY' Alloy C Ni -balPlate & Sheet-ASTM B 334 Mo-16 Sheet Annealed 58 121 47 RB91Rod-ASTM B 336 Cr-16Castings-ASTM A 494 Fe- 5 Sand-Cast Annealed 51 83 9.5 RB93

    W - 4

    HASTELLOY' Alloy 0 Ni -balSi -10 Sand-Cast Annealed 110 110 Rc34Cu- 3

    HASTELLOY* Alloy F Ni -balCr -22 Sheet Annealed 45 103 46 RB86Mo- 6.5Fe-21 Sand-Cast Annealed 37 73 20 RB83Cb & Ta-2

    HASTELLOY* Alloy G Ni -balCr-7 Sheet Annealed 56 103 48 RB87Mo-6.5Fe-5

    HASTELLOY* Alloy N Ni -balCr- 7.0 Sheet Annealed 45 115 51 RB96Fe- 8Ti - 3 Sand-Cast Annealed 40 87 22Mo-16.5

    See page 62 for list of trademarks

    30

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile TorsionalSpecific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btujsq It (68 F) ohms of Elasticity, of Elasticity,Ibjcu in. Specific Gravity F Btujlb;oF in.jinpF jhr;oF jin. jCir mil It in 106 psi x 106 psi Material

    NIMONIC* NICKEL-CHROMIUM ALLOYSNIMONIC*Alloy0.302 8.37 2515 0.11 6.1 7910 65510 32.0 75

    0.297 8.22 2500 0.103 6.2 7010 73210 32.114

    NIMONIC*Alloy80A

    0.296 8.19 2500 0.11 6.4

    NIMONIC*Alloy90

    7510 70810 32.814

    0.284 7.85 2400 0.11 6.2 80310 31.314

    NIMONIC*Alloy115

    HASTELLOY* ALLOYS0.334 9.24 2460 0.091 5.617 723 810 30.9 HASTELLOY*

    Alloy28.5 B

    HASTELLOY*0.323 8.94 2380 0.092 6.317 613 779 29.8 Alloy

    C26.0

    HASTELLOY*0.281 7.80 2050 0.109 6.111 1453 679 28.9 Alloy

    0

    HASTELLOY*0.295 8.17 2350 0.102 8.117 1003 673 29.0 Alloy

    F

    HASTELLOY*0.300 8.34 2400 0.100 1003 Alloy

    G

    HASTELLOY*0.317 8.79 2550 0.100 6.217 713 835 31.714 Alloy

    N

    3=at68 F 10=at 212 F 14= Dynamic Modulus 17 70to200F

    31

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    HASTEllOY* AllOYS (continued)HASTELLOY* Alloy W Cr- 5

    Wire-AMS 5786 Mo-24.5 Sheet Annealed 53 123 55Bar & Forgings-AMS 5755A Fe - 5.5

    Ni -bal

    HASTELLOY* Alloy X Ni -bal(AISI No. 680) Cr -22

    Plate, Sheet, Strip-AMS 55360 Fe -18.5Mo- 9Co- 1.5 max Sheet Annealed 52 114 43 RB90W - 0.60C-maxWrought-O.15Cast -0.20

    HASTELLOY* Alloy R235 Ni -balCr -15.5Fe-lO Sheet Annealed and Aged 117 169 21 Rc32Ti - 2.5AI- 2.0Mo- 5.5

    HIGH TEM PERATU RE- HIGH STRENGTH AllOYSGMR 2350 Alloy Ni -bal

    Cr -15.5Mo- 5.0Fe - 4.5 Casting As Cast 103 112 3.5Ti - 2.5AI- 3.5B - 0.05

    Alloy 713C Ni -balCastings-AMS 5391A Cr -12.5

    Mo- 4.2Cb- 2Ti - 0.8 Casting As Cast 107 123 7.9 Rc34AI - 6.1B - 0.012Zr - 0.10C - 0.12

    Alloy 713LC Ni -balCr -12Mo- 4.5Cb- 2Ti - 0.6 Casti ng As Cast 109 130 15 Rc39AI- 5.9B - 0.01Zr - 0.10C - 0.05

    Alloy 901 Ni -42.5 Bar 2000 FW.Q.(AISI No. 682) Cr -12.5 plus 1460 F A.C.,

    Bar & Forgings-AMS 5660B Mo- 5.7 plus 1225 F A.C. 130 175 14Fe -balTi - 2.8 Sheet 1950 F A.C.,AI- 0.2 plus 1325 F A.C. 107 166 23B - 0.015

    * See page 62 for list of trademarks

    32

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu Isq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F BtujlbrF in.jin.;oF jhr rF jin. jcir mil It in 106 psi x 10 psi Material

    HASTELLOY* ALLOYS (continued)

    HASTELlOY*0.325 9.03 2400 6.31 Alloy

    W

    HASTELLOY*AlloyX

    0.297 8.23 2470 0.116 7.7017 633 712 28.614

    0.296 8.22 2535 0.11 6.711 796 30.514

    HASTELLOY*AlloyR-235

    HIGH TEMPERATURE-HIGH STRENGTH ALLOYS

    GMR2350Alloy

    0.291 8.05 28.714

    Alloy713C

    0.286 7.91 2350 5.9217 14620 29.914

    Alloy713LC

    0.289 8.00 2410 5.9217 14620 28.614 7.4

    ~ AlloyIJ 9010.297 8.22 7.7517 9720 29.914

    1=68 to 212 F 14= Dynamic Modulus 17=70 to 200 F 20=at 200 F

    33

  • Properties OF SOM E METALS AN 0 ALLOYS

    Material

    Typical Mechanical Properties

    Nominal Composition(essential elements).

    %

    YieldStrength

    (0.2% offset).1000psi

    Elongationin 2 in .

    %

    Hardness.Brinell orRockwell

    TensileStrength.1000psi

    Form andCondition

    HIGH T EM PERATU RE - H I G H STR ENGTH A LLOYS (continued)

    Alloy A-286(AISI No. 660)

    Bar-ASTM A461 Grade 660

    Ni -26. Cr -15Mo- 1.3Fe -balTi - 2AI- 0.2B - 0.Dl5

    Bar 1800 F O.Q.plus 1325 F A.C. 105 146 25 Rc28

    IN 100 AlloyCastings-AMS 5397

    Ni -balCr-lOCo-15Mo- 3Ti - 4.7AI- 5.5B - 0.014V-IZr - 0.06

    Cast 123 147 9

    IN 102 Alloy Ni -balCr -15.0Mo- 3W - 3Cb- 3Fe- 7Ti - 0.6.1\1- 0.4B - 0.005Zr - 0.03

    Bar 1800 F A.C. 73 139 47 215

    L-605 Alloy(AISI No. 670)

    Bar & Forgings-AMS 5759C

    Ni -10Cr-20Co-balW -15

    Sheet 2250 F A.C. 67 146 64

    MAR M246 Alloy Ni -balCr - 9Co-InMo- 2.5W -10Ti - 1.5AI- 5.5B - 0.015Ta - 1.5Zr - 0.05

    Cast 125 140 5

    M-252 Alloy(AISI No. 689)

    Bar-ASTM A461 Grade 680

    Ni -balCr -20Co-10Mo-lOTi - 2.6AI - 1.0B - 0.005

    Bar 1900 F A.C.plus 1400 F A.C. 16 Rc39122 180

    RENE 41* Alloy(AISI No. 683)

    Bar & Forgings-AMS 5712A

    Ni -balCr -19Co-lOMo-IOTi - 3.1AI - 1.5B - 0.005

    Bar 1950 F A.C.plus 1400 F A.C. 154 206 14

    * See page 62 10r list of tradema rks

    34

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in/in.;oF

    ThermalConductivity(32 to 212 F),

    Btu/sq ItIhr rF lin.

    ElectricalResistivity,(68 F) ohmslcir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    HI G H TEM P ERAT U RE - H I G H STREN GTH ALLOYS (continued)

    AlloyA-286

    0.286 7.91 2550 0.10 9.1717 10020 546 29.114 10.4

    IN 100Alloy

    0.280 7.75 2435 7.2017 31.214

    IN 102Alloy

    0.309 8.55 2530 7.3217 8620 29.714

    L-6050.330 9.13 2570 0.09 6.8317 7520 32.614 Alloy

    MARM246Alloy

    0.305 8.44 2450

    M-252Alloy

    0.298 8.25 2500 5.917 9020 29.814

    RENE 41*Alloy

    0.298 8.25 2500 0.11 6.6317 6220 31.914

    14=Dynamic Modulus 17=70 to 200 F 20=at200 F

    35

  • Properties OF SOME METALS AND ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinel! or

    Material % Condition 1000 psi 1000 psi % Rockwel!

    HIGH TEMPERATURE-HIGH STRENGTH ALLOYS (continued)

    S816 Alloy Ni -20(AISI No. 671) Cr-20

    Bar-ASTM A461 Grade 671 Co-bal Bar 2150 F A.C.Mo- 4 plus 1400 F A.C. 67 140 35W - 4Cb- 4Fe - 4

    TO Nickel Ni- bal Bar 1800 F A.C. 90 100 25ThO. - 2.2

    U01 MET* Alloy 500 Ni -bal(AISI No. 684) Cr-18

    Bar-ASTM A 461 Grade 684 Co-18.5 Bar 1975 F A.C.Mo- 4 plus 1550 F A.C. 110 176 16Ti - 2.9 plus 1400 F A.C.AI- 2.9Zr - 0.05B - 0.006

    U01MET* Alloy 700 Ni -bal(AISI No. 687) Cr-15 Bar 2150 F A.C.

    Co-18.5 plus 1975 F A.C.Mo- 5.2 plus 1550 F A.C. 140 204 17Ti - 3.5 plus 1400 F A.C.AI- 4.3B - 0.030

    WI52 Alloy Co-balCr -21W -11 Cast 85 109 5 Rc32Cb- 2Fe- 2C - 0.45

    WASPALOY* Ni -bal(AISI No. 685) Cr -19.5

    Bar-ASTM A 461 Grade 685 Co-13.5 Bar 1975 F A.C.Mo- 4.3 plus 1550 F A.C. 115 185 25Ti - 3 plus 1400 F A.C.AI - 1.3B - 0.006Zr - 0.06

    81900 Alloy Ni -balCr - 8Co-IOMo- 6Ti - 1 Casting As Cast 120 141 8AI- 6Ta- 4B - 0.Dl5Zr - 0.10

    0979 Alloy Ni -bal(AISI No. 664) Cr -15

    Bar & Forgings-AMS 5746A Mo- 4 Bar 1900 F O.Q.W - 4 plus 1550 F A.C. 146 204 15Fe-27 plus 1300 F A.C.Ti - 3AI- 1B - 0.01

    * See page 62 for list of trademarks

    36

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in./in.j"F

    ThermalConductivity(32 to 212 F),

    Btu /sq It/hr rF fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    HI G H T EM PER A T U RE - H I G H 5 T RENGT HAL L0 Y 5 (continued)

    S816Alloy

    0.313 8.65 2450 7.3817 8620 34.914 13.6

    0.322 8.90 2650 0.106 6.017 57220 45 22.014 TO Nickel

    UDlMET*Alloy500

    0.290 8.02 2540 6.7517 32.114

    UDlMET*Alloy700

    0.286 7.91 2550 7.7421 13620 32.414

    WI52Alloy

    0.321 8.87 2450 0.11 8.021 17220

    WASPALOY*

    0.296 8.19 2475 6.817 7420 30.914

    81900Alloy

    0.297 8.22 2375 6.5017 7120 31.014

    0979Alloy

    0.296 8.19 2550 7.6017 9220 30.014 11.6

    14~ Dynamic Modulus 17~70 to 200 F 20~at 200 F 21~ 70 to 1000 F

    37

  • Properties OF SOME METALS AND ALLOYS

    Material

    Nominal Composition(essential elements),

    %

    Typical Mechanical Properties

    Form andCondition

    YieldStrength

    (0.2% offset),1000 psi

    Hardness,Brine" orRockwell

    TensileStrength,1000 psi

    Elongationin 2 in.,

    %

    X40 AlloyCastings-AMS 5382

    HI G H T EM PER A T U RE - HI G H ST REN GT HAL L0 YS (continued)Co-balNi -10.5Cr -25.5W - 7.5

    Casting As Cast 76 108 9

    16256 Alloy(AISI No. 650)

    Plate, Sheet, Strip-ASTM A 457 Grade 650

    Forgings-ASTM A 477Bar-ASTM A 458

    Fe -balCr -16Ni -25Mo- 6N - 0.15

    Bar 2150 F W.Q. 51 109 46 187

    N155 Alloy(AISI No. 661)

    Bar-ASTM A 461 Grade 661

    Ni -20Cr -21Co-20Mo- 3W - 2.5Cb- 1Fe -balN 0.15

    Bar 2150 F W.Q.plus 1500 F A.C. 58 118 40 218

    DISCALLOY*(AISI No. 662)

    Bar-ASTM A 461 Grade 662

    Ni -26Cr -13.5Fe -balMo- 2.7Ti - 1.7AI - 0.1B 0.005

    Bar 1850 F O.Q.plus 1500 F A.C.plus 1200 F A.C.

    106 145 19 300

    Ingot Iron

    IRON AND STEEL ALLOYS

    Fe -99.9 plusHot Rolled 29

    19

    45 26

    45

    90

    67Annealed 38

    Wrought IronForgings ASTM A 73

    100>e-balSlag 2.5

    Hot Rolled 48 3030

    Carbon Steel-SA E 1020ASTM A 285

    65Fe -balC - 0.20Mn- 0.45Si 0.25

    Annealed 38 30 130

    Quenched and Temperedat 1000 F 25 17962 90

    300 M Alloy SteelBar & Forgings-AMS 6416

    Fe -balMn- 0.80Si - 1.6Ni - 1.85Cr - 0.85Mo- 3.38V - 0.08C 0.43

    Hardened 240 290 53510

    9% Nickel SteelPlate-ASTM A 553 87 110 37

    Fe -balNi - 9C 0.13 max

    Plate Quenched Tem peredat 1175 F Rc23

    Maraging Steel 18200Plate-ASTM A 538

    Fe balNi -18Mo- 3.2Ti - 0.2AI - 0.1C - 0.03 maxCo 8.5

    Annealed 117 145 17 Rc27

    Rc46Aged at 900 F 200 215 12

    * See page 62 for list of trademarks

    38

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./in.j"F /hr rF fin. /cir mil ft in 106 psi x 106 psi Material

    HIGH TEMPERATURE-HIGH STRENGTH ALLOYS (continued)X-40

    0.311 8.60 8.3921 8220 32.814 Alloy

    16-25-6Alloy

    0.291 8.05 2550 9.621 10820 32.014 11.0

    N-155Alloy

    0.296 8.19 2475 7.7511 9120 559 29.314

    DISCAllOY*

    0.288 7.97 2665 0.113 8.5017 9720 28.414

    IRON AND STEEL ALLOYS

    0.284 7.86 2795 0.108 6.8 490 57 30.1 11.8 Ingot Iron

    0.278 7.70 2750 0.11 6.35 418 70 29 Wrought Iron

    0.284 7.86 2760 0.107 6.7 360 60 30 Carbon Steel-SAE 1020

    300MAlloySteel

    0.283 7.84 2740 0.107 6.7 360 60 30 11.6

    9% Nickel Steel0.284 7.86 2730 0.08822 4.922 9123 203 3023

    MaragingSteel

    2033 273 18-200

    0.289 8.00 2650 0.107 5.624 1363 300 to 420 26.2

    3=a168 F 14=Dynamic Modulus 17=7010200 F 20=a1200 F 21=70 to 1000 F22=from -320 F to RoomTemperature 23=al -32 F 24=R.T. to 900 F

    39

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    IRON AND STEEL ALLOYS (continued)Maraging Steel 18-250 Fe -bal

    Plate-ASTM A 538 Ni -18Mo- 4.8 Annealed 116 146 19 Rc29Ti - 0.4AI - 0.1 Aged at 900 F 250 260 10 Rc49C - 0.03 maxCo- 7.8

    Maraging Steel 18-300 Fe -balPlate-ASTM A 538 Ni -18.5

    Mo- 4.8 Annealed 115 147 17 Rc32Ti - 0.65AI - 0.1 Aged at 900 F 280 290 8 Rc53C - 0.03 maxCo - 8.7

    CAST IRON ALLOYSCast Gray Iron C - 3.4

    ASTM A 48 Class 30 Si - 1.8 As Cast 32 190Mn- 0.8Fe -bal

    Malleable Iron C - 2.5Castings-ASTM A 47 Si - 1 Annealed 33 52 12 130

    Mn- 0.55 maxFe -bal

    Ductile Iron Fe -bal(Nickel Containing) C - 3.6Grade 60-40-18 Si - 2.3 Annealed 47 65 24 160

    Castings-ASTM A 536 Mn- 0.5Ni - 0.75

    Ductile Iron Fe -bal(Nickel Containing) C - 3.6Grade 65-45-12 Si - 2.3 Annealed or As Cast 52 72 13 174

    Castings-ASTM A 536 Mn- 0.5Ni - 0.75

    Ductile Iron Fe -bal(Nickel Containing) C - 3.6Grade 80-55-06 Si - 2.3 As Cast 65 90 8 228

    Castings-ASTM A 536 Mn- 0.5Ni - 0.75

    Ductile Iron Fe -bal(Nickel Containing) C - 3.6Grade 100-70-03 Si - 2.3 Normalized and Tempered 80 110 6 260

    Castings-ASTM A 536 Mn- 0.5Ni - 0.75

    Ductile Iron Fe -bal(Nickel Containing) C - 3.6Grade 120-90-02 Si - 2.3 Oil Quenched and Tempered 120 140 4 325

    Castings-ASTM A 536 Mn- 0.5Ni - 0.75

    Hi- Resist Type 1 Fe -balASTM A436 Ni -15.5

    Si - 2Mn- 1.25 As Cast 27 150Cu- 6.5Cr - 2C - 3 max

    40

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-in./inpF

    ThermalConductivity(32 to 212 F),

    Btu/sq ft/hrrF fin.

    ElectricalResistivity,(68 F) ohms/cir mil ft

    TensileModulus

    of Elasticity,in 10 psi

    TorsionalModulus

    of Elasticity,x 10 psi Material

    IRON AND STEEL ALLOYS (continued)

    MaragingSteel18-250

    27.0

    MaragingSteel18-300

    27.5

    CAST IRON ALLOYS

    Cast Gray Iron0.260 7.20 2150 6.7 310 400 14

    Malleable Iron0.264 7.32 2250 0.122 6.6 180 25

    Ductile Iron

    0.250 7.1 2150 6.21 27610 39911 24.5 9.3

    Ductile Iron

    0.250 7.1 2150 6.21 27610 39911 24.5 9.3

    Ductile Iron

    0.252 7.2 2150 5.91 21810 40811 24.5 9.3

    Ductile Iron

    0.252 7.2 2150 5.91 21810 40811 24.5 9.3

    Ductile Iron

    0.252 7.2 2150 5.91 21810 40811 24.5 9.3

    Ni-ResistType 1

    0.264 7.3 2250 0.116 10.44 276 1020 15.6 4.5

    1=68 to 212 F 4=68 to 392 F 10 =at 212 F

    41

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    CAST IRON ALLOYS (continued)Ni-Resist Type 2 Fe -bal

    ASTM A 436 Ni -20Si - 2 As Cast 27 145Mn- 1.25Cr- 2C - 3 max

    Ni-Resist Type 5 Fe -balASTM A436 Ni -35

    Si - 1.5 As Cast 22 110Mn- 0.6C - 2.4 max

    Ductile Ni-Resist Type 02 Fe -balCastings-ASTM A 439 Ni -20

    Si - 2.25 As Cast 32 59 14 170Cr - 2.75C - 3 max

    Ductile Ni-Resist Type 05 Fe -balCastings-ASTM A 439 Ni -35 As Cast 32 58 30 155

    Si - 2C - 2.4 max

    Ni-Hard Type 1 Fe -balCastings-ASTM A 532 Ni - 4.5 Sand Cast 60 600

    Cr - 2.1C - 3.3 Chill Cast 90 650Si - 0.5Mn- 0.6

    Ni- Hard Type 2 Fe -balCastings-ASTM A 532 Ni - 4.5 Sand Cast 60 575

    Cr - 2.1C - 2.8 Chill Cast 100 625Si - 0.5Mn- 0.6

    Ni- Hard Type 4 Fe -bal(Cast) Ni - 6 Sand Cast 80 600

    Cr - 8.5C - 3.0 Chill Cast 110 650Si - 1.5Mn- 0.6

    DURIRON* Fe -bal(Cast) Si -14.5 As Cast 16 520Iron-Silicon Alloy C - 0.85

    DURICHLOR* Fe-bal(Cast) Si -14.5 As Cast 16 520Iron-Silicon-Molybdenum Alloy Mo- 3

    C - 0.85

    WROUGHT STAINLESS STEELType 201 Stainless Steel Fe -bal

    Plate, Sheet & Strip-ASTM A 412 Cr -178ar-ASTM A 429 Ni - 4.5 Strip Annealed 55 115 60 RB90

    Mn- 6.5N, - 0.25 maxC - 0.15 max

    * See page 62 for list of trademarks

    42

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq ft (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./inpF /hr rF fin. /cir mil It in 106 psi x 106 psi Material

    CAST IRON ALLOYS (continued)

    Ni-ResistType 2

    0.264 7.3 2250 0.116 10.44 276 1020 15.6 4.5

    NiResistType 5

    0.268 7.4 2250 2.84 273 10.5 4.5

    Ductile Ni-ResistType D2

    0.268 7.41 2250 10.44 93 612 17.5

    Ductile Ni- Resist0.278 7.68 2250 18 Type D5

    Ni-Hard0.278 7.70 4.725 9926 4805 25 Type 1

    0.278 7.70 4.725 9926 4805 25Ni-HardType 2

    0.278 7.70 6.425 9926 5405 25NiHardType 4

    DURIRON*0.255 7.0 2300 0.13 7.421 23

    DURICHLOR*0.255 7.0 2300 0.13 7.2 23

    WROUGHT STAINLESS STEEL

    0.283 7.86 8.727 423 28.6

    Type 201StainlessSteel

    4=68 to 392 F 21=70 to 1000 F 25=50 to 200 F 26=at 120 F 27=32 to 700 F

    43

  • Properties OF SOME METALS AN D ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    WROUGHT STAINLESS STEEL (continued)Type 202 Stainless Steel Fe -bal

    Sheet, Plate & Strip-ASTM A 412 Cr -18Bar-ASTM A 314 & A 429 Ni - 5 Strip Annealed 55 105 55 RB90Forgings-ASTM A 473 Mn- 8

    N2- 0.25 maxC - 0.15

    Type 301 Stainless Steel Fe -bal Strip Annealed 40 110 60 RJi85Plate, Sheet & Strip-ASTM A 167 Cr -17 up to up to up to

    Ni - 7 Cold Rolled 165 200 8 Rc41C - 0.15 max

    Type 302 Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal Sheet Annealed 40 90 50 RB85& A240 Cr -18 up to up to up to

    Bar-ASTM A 276 & A 314 Ni- 9 Cold Rolled 165 190 5 Rc40Wire-ASn~ A 313 C - 0.15 maxForgings-ASTM A 473

    Type 303 & 303 Se Stainless Steel Fe -balBar-ASTM A 276 & A 314 Cr -18Forgings-ASTM A 473 Ni - 9 Bar Annealed 35 90 50 160

    fS - 0.15 min or'[Se - 0.15 minC - 0.15 max

    Type 304 Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal Sheet Annealed 35 85 50 RB80& A 240 Cr -18.5 up to up to up to

    Tube-ASTM A 213 & A 249 Ni - 9.5 Cold Rolled 160 185 4 Rc40Bar-ASTM A 276 & A 314 C - 0.08 maxForgings-ASTM A 473

    Type 304l Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal& A 240 Cr -18.5 Sheet Annealed 28 75 50 RB70

    Tube-ASTM A 213 & A 249 Ni -10Bar-ASTM A 276 & A 314 C - 0.03 maxForgings-ASTM A 473

    Type 304 plus Boron Stainless Steel Fe -balCr -18 Sheet Annealed 53 96 12 RB95Ni -10B-2

    Type 305 Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal& A 240 Cr -18 Sheet Annealed 38 85 50 RB80

    Tube-ASTM A 249 Ni -12Bar-ASTM A 314 C - 0.l2 maxForgings-ASTM A 473

    Type 309 Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal& A 240 Cr -23 Sheet Annealed 45 90 45 RB85

    Tube-ASTM A 249 Ni -13.5Bar-ASTM A 276 & A 314 C - 0.20 maxForgings-ASTM A 473

    Type 310 Stainless SteelPlate, Sheet & Strip-ASTM A 167 Fe -bal& A 240 Cr -25 Sheet Annealed 45 95 45 RB85

    Tube-ASTM A 213 & A 249 Ni -20Bar-ASTM A 276 & A 314 C - 0.25 maxForgings-ASTM A 473

    44

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-in./in.;oF

    ThermalConductivity(32 to 212 F),

    Btu/sq It/hr rF fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 10 psi

    TorsionalModulus

    of Elasticity,x 10 psi Material

    iN R0 UGH T ST A I N L ESS S TEE L (continued)

    0.282 7.83 10.228

    Type 202Stainless

    427 Steel

    0.29 7.9 2590 0.12 9.4 11310 432 28 12.5 Type 301StainlessSteel

    Type 3020.29 7.9 2590 0.12 9.6 11310 432 28 12.5 Stainless

    Steel

    Type 303 &303 Se

    0.29 2590 0.12 9.6 11310 432 28 StainlessSteel

    Type 3040.29 7.9 2650 0.12 9.6 11310 432 28 12.5 Stainless

    Steel

    0.29 7.9 2650 0.12 9.6 11310 432 28 12.5

    Type 304LStainlessSteel

    Type 3040.29 0.12 10.529 445 plus Boron

    StainlessSteel

    Type 305Stainless

    0.29 2650 0.12 9.6 11310 432 28 12.5 Steel

    0.29 7.9 2650 0.12 8.3 9610 468 29

    Type 309StainlessSteel

    0.29 7.9 2650 0.12 8.0 9610 468 30

    Type 310StainlessSteel

    10=at 212 F 28=32 to 600 F 29=32 to 1200 F

    45

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    WROUGHT STAINLESS STEEL (continued)Type 314 Stainless Steel Fe -bal

    Bar-ASTM A 276 & A 314 Cr -25Ni -20 Bar Annealed 50 !OO 45 180Si - 2.50C - 0.25 max

    Type 316 Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 167 Cr -17

    & A 240 Ni -12 Sheet Annealed 40 90 50 RB85Tube-ASTM A 213 & A 249 Mo- 2.25Bar-ASTM A 276 & A 314 C - 0.08 maxForgings-ASTM A 473

    Type 316L Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 167 Cr-17

    & A 240 Ni -13 Sheet Annealed 32 75 50 RB72Tube-ASTM A 213 & A 249 Mo- 2.25Bar-ASTM A 276 & A 314 C - 0.03 maxForgings-ASTM A 473

    Type 317 Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 167 Cr -19

    & A 240 Ni -14 Sheet AnnealedMo- 3.25C - 0.08 max

    Type 321 Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 167 Cr -18

    & A 240 Ni -11 Sheet Annealed 35 90 50 RB80Tube-ASTM A 213 & A 249 Ti - 5xC minBar-ASTM A 276 & A 314 C - 0.08 maxForgings-ASTM A 473

    Type 330 Stainless Steel Fe -bal Hot Roiled 55 100 35 200Plate, Sheet & Strip-AMS 5592 Cr -15

    Ni -35 Annealed 35 80 50 150C - 0.25 max

    Type 347 Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 167 Cr -18

    & A240 Ni -11 Sheet Annealed 40 95 45 RB85Tube-ASTM A 213 & A 240 Ti - 5xC min (321)Bar-ASTM A 276 & A 314 Cb & Ta-lOxC minForgings-ASTM A 473 C - 0.08 max

    12-12 Stainless Steel Fe -balCr -12 Sheet Annealed 32 85 50 145Ni -12

    CARPENTER* No. 10 Stainless Steel Fe -balWire-ASTM A 493 Cr -16 Annealed 29 74 50 126

    Ni -18C - 0.08 max

    CARPENTER* No. 20 Stainless Steel Fe -balNi -29Cr-20 Bar Annealed 35 85 50 160Mo- 2.5Cu- 3.5

    CARPENTER* 20Cb-3 Stainless Steel Fe -balNi-34Cr-20 Bar Annealed 40 90 50 160Mo- 2.5Cu- 3.5Cb- 0.6

    * See page 62 for list of trademarks

    46

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./inpF /hrrF fin. fcir mil It in 106 psi x 106 psi Material

    WROUGHT STAINLESS STEEL (continued)Type 314

    Stainless0.279 0.12 8.428 12110 462 29 Steel

    Type 316Stainless

    0.29 8.0 2550 0.12 8.9 11310 444 28 Steel

    0.29 8.0 2550 0.12 8.9 11310 444 28

    Type 316LStainlessSteel

    Type 317Stainless

    0.29 2550 0.12 8.9 11310 444 28 Steel

    Type 321Stainless

    0.29 2600 0.12 9.3 11210 432 28 Steel

    0.284 7.86 2515 0.11 6.3 9010 600 Type 330StainlessSteel

    Type 347Stainless

    0.29 2600 0.12 9.3 11210 438 28 Steel

    12120.289 8.01 10.01 1073 420 Stainless

    Steel

    CARPENTER*0.29 0.12 9.5 476 No.10

    StainlessSteel

    CARPENTER*NO.20

    0.289 8.02 0.12 7.861 451 28 10.5 StainlessSteel

    CARPENTER*20Cb3

    0.291 8.03 0.12 8.311 625 28 11 StainlessSleel

    1=68 to 212 F 3=at 68 F 10=at 212 F 28=32 to 600 F

    47

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    WROUGHT STAINLESS STEEL (continued)189 LW* Stainless Steel Fe -bal

    Cr -18 Annealed 30 78 65 150Ni - 9Cu- 2

    177 PH* Stainless Steel Fe -bal Sheet Solution Treated 40 130 35 RB85(AISI No. 631) Cr-17

    Bar-ASTM A 461 Grade 631 Ni - 7 Hardened 220 235 6 Rc48AI - 1.1

    174 PH* Stainless Steel Fe -bal(AISI No. 630) Cr -16.5 Bar Solution Treated 110 150 12 Rc32

    Bar-ASTM A 461 Grade 630 Ni - 4Cu- 4 Hardened 185 200 14 Rc44Cb & Ta-OJ

    155 PH* Stainless Steel Fe -bal Ba r Sol ution Treated 110 150 12 Rc32Bar-AMS 5659A Cr-15

    Ni - 5 Hardened 185 200 14 Rc44Cu- 4

    PH 157 Mo Stainless Steel Fe -bal(AISI No. 632) Cr -15 Solution Treated 55 130 35 RB88

    Bar-ASTM A 461 Grade 632 Ni - 7Mo- 2.5 Hardened 225 240 6 Rc48AI - 1.1

    PH 148 M0* Stai n less Steel Fe-balCr -14 Sheet Solution Treated 55 125 25 RB88Ni - 8Mo- 2.5 Hardened 220 235 5 Rc49AI - 1.1

    PH 138 Mo Stainless Steel Fe -balCr-13 Bar Solution Treated 100 160 15 Rc30Ni - 8Mo- 2.2 Hardened 200 225 13 Rc48AI- I

    Stainless" W"* Fe -bal(AISI No. 635) Cr -17 Annealed 98 135 15 Rc26

    Ni - 7Ti - 0.7 Hardened at 1000 F 190 200 11 Rc44AI- 0.2C - 0.07

    AM 350* Stainless Steel Fe -bal(AISI No. 633) Cr -17 Annealed 60 145 40 290

    Sheet & Strip-AMS 5546 Ni - 4Tube-AMS 5554 Mo- 3 Hardened 173 206 13.5 410

    C - 0.08

    AM 355* Stainless Steel Fe -bal Annealed 57 160 26 310(AISI No. 634) Cr -15.5

    Bar-ASTM A 461 Grade 634 Ni - 4.5 Hardened 174 210 14 415Mo- 3

    CUSTO M 455* Stainless Steel Fe -bal(Maraging) Cr -11.75

    Ni - 9 Annealed 115 140 12 280Cu- 2.25Ti - 1.2 Hardened 220 230 10 500Cb- OJC - 0.03 max

    * See page 62 for list of trademarks

    48

  • Typical Physical Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lbrF in./in.;oF /hrrF/in. /cir mil It in 106 psi x 106 psi Material

    WROUGHT STAINLESS STEEL (continued)189 LW*

    StainlessSteel

    0.282 7.81 8.517 480 177 PH*Stainless

    0.276 7.65 5.717 12818 498 29 11 Steel

    174 PH*0.280 7.78 0.11 6.017 588 Stainless

    Steel0.282 7.80 0.10 6.017 13518 462 28.5 12.7

    0.280 7.78 0.11 6.017 588 28.5 11.2 155 PH*Stainless

    0.282 7.80 0.10 6.017 13518 462 Steel

    PH 157 Mo*0.282 7.80 8.017 480 Stainless

    Steel0.277 7.68 5.017 11220 498 29 11.4

    PH 148 Mo*0.283 7.82 Stainless

    Steel0.278 7.71 5.317

    PH 138 Mo*StainlessSteel

    Stai nless" W"*0.28 7.65 5.5 13010 600 28

    0.28 7.65 14510 510 28 11.3

    AM 350*0.286 7.92 2550 Stainless

    Steel0.282 7.81 6.3 100 475 29.4 11.3

    0.286 7.92 2550 AM 355*Stainless

    0.282 7.81 6.4 105 455 29.3 11.4 Steel

    CUSTOM 455*Stainless

    0.280 7.7 5.9 29 11 Steel

    10=at 212 F 17=70 to 200 F 18=at 500 F 20=at 200 F

    49

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwall

    WROUGHT STAINLESS STEEL (continued)AM 363* Stainless Steel Fe -bal

    Cr -11.5 Strip Annealed and Aged 106 123 12Ni - 4.5Ti - 0.4

    1714 Cu Mo* Stainless Steel Fe -bal(AISI No. 653) Cr-17

    Ni -14 Annealed and Aged 42 86 45 170Cu- 3Mo- 2.5 Hot Cold Worked 20% 93 114 20 255Ti - 0.25Cb- 0.5

    2169 Stainless Steel Fe -balCr -21 Annealed 70 115 42 190Ni - 6Mn- 9

    199 OL Alloy Fe -bal(AISI No. 651) Cr -19 Hot Rolled

    Plate, Sheet & Strip-ASTM A 457 Ni - 9 and Stress Relieved 41 74 30 216Bar-ASTM A 458 Mo-lForgings-ASTM A 477 Grade 651 W - 1.25 Cold Worked

    Cb & Ta-O.40 and Stress Relieved 88 98 13 321Ti - 0.25C - 0.30

    199 OX Alloy Fe -bal(AISI No. 652) Cr-19 Hot Rolled

    Plate, Sheet & Strip-ASTM A 457 Ni - 9 and Stress Relieved 41 74 30 216Bar-ASTM A 458 Mo- 1.5Forgings-ASTM A477 Grade 652 W - 1.25 Cold Worked

    Ti - 0.60 and Stress Relieved 88 98 13 321C - 0.30

    Greek Ascoloy Stainless Steel Fe -bal(AISI No. 615) Cr -12 Bar Hardened 150 170 13 340AMS 5616 W - 3

    Ni - 2

    Type 405 Stainless Steel Fe -balPlate, Sheet & Strip-ASTM A 176 Cr -12.5

    & A 240 C - 0.08 max Sheet Annealed 40 65 25 RB75Tube-ASTM A 268 AI - 0.20Bar-ASTM A 276 & A 314

    Type 410 Stainless SteelPlate, Sheet & Strip-ASTM A 176 Fe -bal Sheet Annealed 45 70 25 RB80

    & A 240 Cr -12Tube-ASTM A 268 C - 0.l5 max Heat Treated 140 180 15 Rc39Bar-ASTM A 276 & A 314Forgings-ASTM A 473

    Type 414 Stainless Steel Fe -bal Sheet Annealed 105 120 15 RB98Bar-ASTM A 276 & A 314 Cr -12.5Forgings-ASTM A 473 Ni - 2 Bar Heat Treated 150 200 15 Rc43

    C - 0.l5 max

    Type 420 Stainless Steel Fe -bal Bar Annealed 50 95 25 RB92Bar-ASTM A276 & A 314 Cr -13Forgings-ASTM A 473 C -over 0.l5 Heat Treated 195 230 8 500

    * See page 62 for list of trademarks

    50

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbrF

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6in./in,rF

    ThermalConductivity(32 to 212 F),Btu/sq It/hr rF fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    WROUGHT STAINLESS STEEL (continued)

    0.281 2650 5.7 27.9 10.6AM 363'

    StainlessSteel

    0.287 8.01 8.23 98 28

    17-14 Cu Mo'StainlessSteel

    21-6-96.3 96 28 Stainless

    Steel

    19-9OL

    0.287 7.94 2615 0.10 8.5 94 29.5 Alloy

    0.287 7.94 2615 0.10 8.5 94 29.5

    19-9OXAlloy

    Greek0.284 7.86 2670 0.11 5.3 29 Ascoloy

    StainlessSteel

    Type 405Stainless

    0.28 7.7 2790 0.11 6.0 360 29 Steel

    Type 4100.28 7.7 2790 0.11 6.1 17310 342 29 Stainless

    Steel

    0.28 0.11 5.8 17310 420 Type 414StainlessSteel

    0.28 7.7 0.11 5.7 17310 330 29 Type 420StainlessSteel

    10=.1212 F

    51

  • Properties OF SOME METALS AND ALLOYS

    Material

    Nominal Composition(essential elements),

    %Form andCondition

    Typical Mechanical Properties

    YieldStrength

    (0.2% offset),1000 psi

    TensileStrength,1000 psi

    Elongationin 2 in.,

    %

    Hardness,Brinell orRockwell

    W RO UGH T STAI N LESS ST EEL (continued)

    Type 430 Stainless SteelPlate, Sheet & Strip-ASTM A 176

    & A 240Tube-ASTM A 268Bar-ASTM A 276 & A314Forgings-ASTM A473

    Fe -balCr -17C - 0.12 max

    Sheet Annealed

    Cold Rolled

    45up to95

    75up to110

    25

    10

    RB80up to225

    Type 431 Stainless SteelForgings-ASTM A473Bar-ASTM A276 & A 314

    Fe -balCr -16Ni - 1.75C - 0.20 max

    Bar Annealed

    Hardened

    95

    150

    125

    195

    25

    15

    260

    400

    Type 440C Stainless SteelForgings-ASTM A 473Bar-ASTM A276 & A314

    Fe -balCr -17C - 1.10

    Bar Annealed

    Quenched and Tempered 600 F

    65 110 14

    2

    230

    275 285 Re57

    Type 446 Stainless Steel- Plate, Sheet & Strip-ASTM A 176

    Tube-ASTM A 268Bar-ASTM A 276 & A 314

    Fe -balCr-25C - 0.20 maxN - 0.25 max

    Sheet Annealed 50 80 20 RB83

    CAST STAINLESS STEEL AND HEAT RESISTING ALLOYS

    CA-15 Cast Stainless SteelGen. Applications-ASTM A 296Valves, Fittings-ASTM A351

    Fe -balCr -12C - 0.15 max

    1800 F, Air Cooled,Tempered at 600 F

    Tempered at 1400 F

    150 200 7 390

    20075 100 20

    CA-40 Cast Stainless SteelGen. Applications-ASTM A 296 165 470

    212

    Fe -balCr -12C - 0.30

    1800 F, Air Cooled,Tempered at 600 F

    Tem pered at 1400 F

    220

    11067 18

    CB-30 Cast Stainless SteelGen. Applications-ASTM A 296 195

    Fe -balCr -20Ni - 2 maxC - 0.30 max

    Annealed 60 95 15

    CC-50 Cast Stainless SteelGen. Applications-ASTM A 296

    212Fe -balCr-28Ni - 4 maxC - 0.50 max

    As Cast

    1900 F, Air Cooled

    65 70 2

    65 18 21097

    CE-30 Cast Stainless SteelGen. Applications-ASTM A 296

    Fe -balCr -28Ni - 9

    As Cast

    2000 F, Water Quenched

    60

    63

    15

    18

    95

    97

    170

    170

    CF-3 Cast Stainless SteelGen. Applications-ASTM A 296Valves, Fittings-ASTM A 351

    Fe -balCr -19Ni -10C - 0.03 max

    2000 F, Water Quenched 32 13372 55

    CF-8 Cast Stainless SteelGen. Applications-ASTM A296Valves, Fittings-ASTM A351Centrifugal Pipe-ASTM A 451

    Fe -balCr -19Ni - 9C - 0.08 max

    2000 F, Water Quenched 37 77 55 140

    CF-3M Cast Stainless SteelGen. Applications-ASTM A296Valves, Fittings-ASTM A351

    Fe -balCr -19Ni -11Mo- 2.5C - 0.03 rnax

    2000 F, Water Quenched 40 83 50

    52

  • Typical Physical Properties

    Density,Ib/cu in.

    Melting Point,Specific Gravity F

    Specific Heat(32 to 212 F),Btu/lbj"F

    Thermal Expan-sion Coefficient(32 to 212 F),

    in 10-6io./inpF

    ThermalConductivity(32 to 212 F),

    Btu/sq ft/hr j"F fin.

    ElectricalResistivity,(68 F) ohms/cir mil It

    TensileModulus

    of Elasticity,in 106 psi

    TorsionalModulus

    of Elasticity,x 106 psi Material

    WROUGHT STAINLESS STEEL (continued)0.280 7.75 2750 0.11 5.8 18110 360 29

    Type 430StainlessSteel

    0.280 7.78 2700 0.11 6.5 14010 432 29 Type 431StainlessSteel

    0.280 7.75 2700 0.11 5.6 16810 360 29 Type 440CStainlessSteel

    Type 4460.270 7.45 2750 0.012 5.8 14510 402 29 Stainless

    Steel

    CAST STAINLESS STEEL AND HEAT RESISTING ALLOYSCA-15 Cast

    0.275 7.61 2750 0.11 5.51 17410 468 29 Stainless6.421 Steel

    CA-40 Cast0.275 7.61 2725 0.11 5.51 17410 456 29 Stainless

    6.421 Steel

    C8-30 Cast0.272 7.53 2725 0.11 5.71 15410 456 29 Stainless

    6.521 Steel

    0.272 7.53 2725 0.12 5.91 15110 462 29 CC-50 Cast6.421 Stainless

    Steel

    0.277 7.67 2650 0.14 9.621 510 25 CE-30 CastStainlessSteel

    CF-3 Cast0.280 7.75 2600 0.12 9.01 11010 457 Stainless

    10.021 Steel

    CF-8 Cast0.280 7.75 2600 0.12 9.01 11010 457 28 Stainless

    10.021 Steel

    CF-3M CastStainless

    0.280 7.75 2550 0.12 8.91 11310 492 Steel9.721

    1=68 to 212 F 10=at 212 F 21= 70 to 1000 F

    53

  • Properties OF SOME METALS AN 0 ALLOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000 psi 1000 psi % Rockwell

    CAST STAINLESS STEEL AND HEAT RESISTING ALLOYS (continued)CF8M Cast Stainless Steel Fe -bal

    Gen. Applications-ASTM A296 Cr -19Valves, Fittings-ASTM A351 Ni -10 2000 F, Water Quenched 42 80 50 163Centrifuga I Pipe-ASTM A451 Mo- 2.5

    C - 0.08 max

    CF8C Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr -19Valves, Fittings-ASTM A 351 Ni -10Centrifugal Pipe-ASTM A451 C - 0.08 max 2000 F, Water Quenched 38 77 39 149

    Cb- 8xC minor

    Cb & Ta-l0xC min

    CF16F Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr -19

    Ni -10 2000 F, Water Quenched 40 77 52 150S - 0.3Mo- 0.6C - 0.16 max

    CF20 Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr-19 2000 F, Water Quenched 36 77 50 163

    Ni - 9C - 0.20 max

    CG8M Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr -19

    Ni -11 2000 F, Water Quenched 40 83 50Mo- 3.5C - 0.08 max

    CH20 Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr-24 2000 F, Water Quenched 50 88 38 190Centrifugal Pipe-ASTM A451 Ni -13

    C - 0.20 max

    CK20 Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr -25 2100 F, Water Quenched 38 76 37 144Valves, Fittings-ASTM A351 Ni -20Centrifugal Pipe-ASTM A451 C - 0.20 max

    CN7M Cast Stainless Steel Fe -balGen. Applications-ASTM A296 Cr-20Valves, Fittings-ASTM A351 Ni -29 2050 F, Water Quenched 31.5 69 48 130

    Mo- 2Cu- 3 minC - 0.07 max

    CD4M Cu Cast Stainless Steel Fe-balCr-26

    240Ni - 5.5 2050 F, Water Quenched 80 110 20Mo- 2.5Cu- 3.0

    HA Cast Heat Resistant Alloy Fe -bal Annealed 1825 F 65 95 23 180

    Valves, Fittings-ASTM A217 Cr - 9 and :Mo- 1 Aged at 1400 F 81 107 21 220C - 0.20 max

    HC Cast Heat Resistant Alloy Fe -bal As Cast 65 70 2190

    Gen. Applications-ASTM A297 Cr-28 230Ni - 4 max Aged at 1400 F 80 115 18C - 0.50 max

    54

  • Typica I Physica I Properties

    Thermal Expan- Thermalsion Coefficient Conductivity Electrical Tensile Torsional

    Specific Heat (32 to 212 F), (32 to 212 F), Resistivity, Modulus ModulusDensity, Melting Point, (32 to 212 F), in 10-6 Btu/sq It (68 F) ohms of Elasticity, of Elasticity,Ib/cu in. Specific Gravity F Btu/lb/"F in./inpF /hr /"F fin. /cir mil ft in 106 psi x 106 psi Material

    CAST STAINLESS STEEL AND HEAT RESISTING ALLOYS (continued)CF-SM Cast

    Stainless0.280 7.75 2550 0.12 8.91 11310 492 28 Steel

    9.721

    CF-SC CastStainlessSteel

    0.280 7.75 2600 0.12 9.31 11210 426 2810.321

    CF-16F CastStainless

    0.280 7.75 2550 0.12 9.01 11310 432 28 Steel9.921

    CF20 Cast0.280 7.75 2575 0.12 9.61 11010 468 28 Stainless

    10.421 Steel

    CG-SM CastStainless

    0.280 7.75 2550 0.12 8.91 11310 492 Steel9.721

    CH-20 Cast0.279 7.72 2600 0.12 8.31 9810 504 28 Stainless

    9.621 Steel

    CK20 Cast0.280 7.75 2600 0.12 8.01 9810 540 29 Stainless

    9.221 Steel

    CN7M CastStainless

    0.289 8.00 2650 0.11 8.61 14510 538 24 Steel9.721

    CO-4M Cu CastStainless

    6.51 Steel7.121

    0.279 7.72 2750 0.11 6.11 18210 420 29 HA Cast Heat7.121 Resistant

    Alloy

    0.272 7.53 2725 0.12 6.321 151 462 29 HC Cast HeatResistantAlloy

    1=6810212 F 10=al 212 F 21= 7010 1000 F

    55

  • Properties OF SOME METALS AND AllOYSTypical Mechanical Properties

    YieldNominal Composition Strength Tensile Elongation Hardness,(essential elements), Form and (0.2% offset), Strength, in 2 in., Brinell or

    Material % Condition 1000psi 1000psi % Rockwell

    CAST STAINLESS STEEL AND HEAT RESISTING ALLOYS (continued)HD Cast Heat Resistant Alloy Fe -bal

    Gen. Applications-ASTM A 297 Cr-28 As Cast 48 85 16 190Ni - 5.5C - 0.50 max

    HE Cast Heat Resistant Alloy Fe -bal As Cast 45 95 20 200Gen. Applications-ASTM A 297 Cr-28

    Ni - 9 Aged at 1400 F 55 90 10 270C - 0.35

    H F Cast Heat Resistant Alloy Fe -bal As Cast 45 85 35 165Gen. Applications-ASTM A 297 Cr -21

    Ni - 9 Aged at 1400 F 50 100 25 190C - 0.30

    HH Cast Heat Resistant Alloy Fe -bal As Cast 50 80 25 185Gen. Applications-ASTM A 297 Cr -26Structural Parts-ASTM A 447 Ni -12 Aged at 1400 F 55 86 11 200

    C - 0.35

    HI Cast Heat Resistant Alloy Fe -bal As Cast 45 80 12 180Gen. Applications-ASTM A 297 Cr-28

    Ni -16 Aged at 1400 F 65 90 6 200C - 0.35

    HK Cast Heat Resistant Alloy Fe -bal As Cast 50 75 17 170Gen. Applications-ASTM A 297 Cr-26

    Ni -20 Aged at 1400 F 50 85 10 190C - 0.40

    HL Cast Heat Resistant Alloy Fe -balGen. Applications-ASTM A 297 Cr-30 As Cast 52 82 19 192

    Ni -20C - 0.40

    HN Cast Heat Resistant Alloy Fe -balGen. Applications-ASTM A297 Cr -21 As Cast 38 68 17 160

    Ni -25C - 0.35

    HT Cast Heat Resistant Alloy Fe -bal As Cast 40 70 10 180Gen. Applications-ASTM A 297 Cr -15Structural Parts-ASTM A 448 Ni -35 Aged at 1400 F 45 75