TECHNICAL DATA


Table of Contents


Please note. We have provided this technical information on refractory metals to our customers for several years without charge. It has been compiled from what we believe are reliable sources. Indeed, we use it in our daily decision making. However, if you use this in your decision making, you must independently verify that it is correct and that it properly applies to your intended use.


Refractory Metals: Typical Analysis

ElementMaximum % MolybdenumMaximum % TungstenMaximum % TantalumMaximum % Niobium
Aluminum0.0010.002---0.005
Calcium0.0030.003------
Chromium0.0050.002------
Copper0.0010.002------
Iron0.0050.0030.0100.01
Lead0.0020.002------
Magnesium0.0010.002------
Molybdenum99.95 Min---0.0100.01
Manganese0.0010.002------
Nickel0.0010.0030.0050.005
Silicon0.0030.0020.0050.005
Tin0.0030.002------
Titanium0.0020.0020.005---
Tantalum------99.90 Min0.2
Tungsten---99.95 Min0.0300.05
Carbon0.0050.0050.00750.01
Oxygen------0.0200.025
Nitrogen------0.00750.01
Hydrogen------0.00010.0015
Niobium------0.05099.9


Typical Properties of Molybdenum, Tantalum, Tungsten

(Ranges only: Data will vary with type of sample and previous work history)

MolybdenumTungstenTantalum
PropertyAtomic Number427473
Atomic Weight95.95183.86180.95
Atomic Volume9.419.5310.90
Lattice TypeBody centered cubeBody centered cubeBody centered cube
Lattice Constant;
20°C, A
3.14683.15853.3026
Isotope (Natural)92, 94, 95, 96, 97, 98, 100180, 182, 183, 184 186181
MassDensity at 20° C gm/cc10.219.316.6
Density at 20° C lb/in30.3680.6970.600
Thermal PropertiesMelting Point, °C261034102996
Boiling Point, °C556059006100
Linear Coefficient of Expansion per °C4.9 x 10-64.3 x 10-66.5 x 10-6
Thermal Conductivity at 20°C, cal/cm2/cm°C/sec.0.350.400.130
Specific Heat, cal/g/°C; 20°C0.0610.0320.036
Electrical PropertiesConductivity, % IACS30%31%13%
Resistivity, microhms-cm; 20°C5.75.513.5
Temperature Coefficient of Resistivity per °C (0-100°C)0.00460.00460.0038
Mechanical PropertiesTensile Strength at room temperature, psi100,000-200,000100,000-500,00035,000-70,000
Tensile Strength-500°C psi35,000-65,00075,000-200,00025,000-45,000
Tensile Strength-1000°C psi20,000-30,00050,000-75,00013,000-17,000
Young's Modulus of Elasticity; lb/in2
Room Temperature46 x 10659 x 10627 x 106
500°C41 x 10655 x 10625 x 106
1000°C39 x 10650 x 10622 x 106
Spectral Emissivity(Wave Length approx. 0.65)0.37 (1000°C)0.45 (900°C)0.46 (900°C)
Working Temperature1600°C1700°CRoom
Recrystallizing Temp900-1200°C1200-1400°C1000-1250°C
Stress Relieving Temp800°C1100°C850°C
MetallographyEtchantHot H2O2; 6% solHF-NH; F solAlk.K3FE(CN) sol
PolishingAlumina - Rouge to finish
Note: Etch and polish repeatedly until grain boundaries appear.


  Data on Molybdenum

 


 

  Data on Molybdenum and Tungsten


Corrosion Data

General

Corrosion resistance of the refractory metals is second only to that of the noble metals. Unlike the noble metals, however, the refractory metals are inherently reactive.

Such reactivity is a decided plus for corrosion resistance. On contact with air or any other oxidant, refractory metals immediately form an extremely dense, adherent oxide film. This passivating layer prevents access of the oxidant to the underlying metal and renders it resistant to further attack.

Unfortunately, these oxides spall or volatize at elevated temperatures, leaving the metals susceptible to oxidation at approximately 300 to 500 degrees C. For high-temperature applications under non-reducing conditions, the refractory metals must be protected by an applied coating, such as a metal silicide.

Tantalum

Tantalum is clearly the top of the line for corrosion resistance. The only media that can affect it are fluorine, hydrofluoric acid, sulfur trioxide (including fuming sulfuric acid), concentrated strong alkalis, and certain molten salts.

The corrosion resistance of tantalum can be compared to that of glass, although tantalum withstands higher temperatures and offers the intrinsic fabrication advantages of a metal. Tantalum equipment is frequently used in conjunction with glass, glass-lined steel, and other nonmetallic materials of construction. Tantalum is also used extensively to repair damage and flaws in glass-lined steel equipment.

Because of its high cost and lack of strength compared to its easy fabricability, tantalum is usually used as a lining over a stronger, less expensive base material.

Niobium (or Columbium)

Niobium can be a less-expensive alternative to tantalum. However, its corrosion resistance is more limited. This is because it is sensitive to most alkalis and certain strong oxidants.

Niobium does remain totally resistant to such highly corrosive media as wet or dry chlorine, bromine, saturated brines, ferric chloride, hydrogen sulfide, sulfur dioxide, nitric and chromic acids, and sulfuric and hydrochloric acids within specific temperature and concentration limits.

Even though the mechanical strength of niobium is less than that of tantalum, it can be used economically where the extreme inertness of tantalum is not required.

Molybdenum

Molybdenum provides corrosion resistance that is slightly better than that of tungsten. It particularly resists non-oxidizing mineral acids.

Molybdenum is relatively inert to carbon dioxide, hydrogen, ammonia and nitrogen to 1100 degrees C and also in reducing atmospheres containing hydrogen sulfide.

It has excellent resistance to corrosion by iodine vapor, bromine, and chlorine up to clearly defined temperature limits. Molybdenum also provides good resistance to several liquid metals including bismuth, lithium, potassium, and sodium.

For more specific information on refractory metals and the affect of specific reagents, refer to the tables inluded herein.


Chemical Reactivity of Molybdenum

ReagentRVRNRReagentRVRNR
WaterX  HydrogenX  
Hydroflouric Acid1X  NitrogenX  
Hydrochloric Acid (cold)X  Inert Gasses (all)X   
Sulfuric Acid (hot) X Carbon Monoxide (1400°C)-Carbide Formation  X
Nitric Acid (cold) X Carbon Dioxide (1200°C)-Oxidation  X
Nitric Acid (hot)  XHydrocarbons (1100°C)-Carbide Formation  X
Aqua Regia (cold) X Aluminum (molten)  X
Aqua Regia (hot)  XIron (molten)  X
Nitric/Hydroflouric mixture1  XCobalt (molten)  X
Aqueous Ammonia X Nickel (molten)  X
Aqueous Caustic Soda/PotashX  Tin (molten)  X
Molten Caustic X Zinc (molten) X 
Molten Caustics2  XLead X 
Boron (hot)-Boride fomation  XCesium X 
Carbon (1100°C)-Carbide Formation  XGallium X 
Silicon (1000°C)-Silicide Formation  XPotassium X 
PhosphorousX  Lithium X 
Sulfide Formation (440°C)  XMagnesium X 
IodineX  Sodium X 
BromineX  Mercury X 
ChlorineX  BismuthX  
Flourine (room temperature)  XKNO2, KNO3, KCLO3 (molten)  X
Oxygen or air (>400°C) X Molten GlassX  
Oxygen or air (>600°C)  XAl2O3, BeO, MgO, ThO2, ZrO2(<1700°C)X  
Notes: Key:
1. May be either hot or cold.

2. Molten Caustics are in the presence of KNO2, KNO3, KCLO3, PbO2.

R = Resistant.

VR = Variable Resistance depending on temperature and concentration.

NR = Non-resistant.


Chemical Reactivity of Tungsten

ReagentRVRNRReagentRVRNR
WaterX  Flourine  X
Water Vapor (red heat)-Oxidation  XOxygen or air (<400°C)X  
Hydroflouric AcidX  Oxygen or air (>400°C) X 
Hydrochloric AcidX  In air X 
Sulfuric Acid X HydrogenX  
Nitric AcidX  NitrogenX  
Aqua Regia (cold)X  Carbon Monoxide (<800°C)X  
Aqua Regia (warm/hot)  XCarbon Monoxide (>800°C) X 
Nitric/Hydroflouric mixture  XCarbon Dioxide (>1200°C)-Oxidation  X
Aqueous Caustic Soda/PotashX  Aluminum oxide-Oxidation  X
AmmoniaX  Magnesium Oxide-Oxidation  X
Ammonia in presence of H2O2 X Thorium oxide (>2220°C)-Oxidation  X
Ammonia (<700°C)X  Sodium Nitrite (molten)  X
Ammonia (>700°C) X Sulfur (molten, boiling) X 
Carbon (>1400°C)-Carbide Formation  XHydrogen/Chloride Gas (<600°C)X  
Iodine (at red heat)  XNitric Oxide (hot)-Oxidation  X
Bromine (at red heat)  XHydrogen Sulfide (red heat) X 
Chlorine (>250°C) X Sulfur Dioxide (red heat)  X
Carbon Disulfide (red heat)  XIn presence of KNO2, KNO3, KCLO3, PbO2  X
Mercury (and vapor)X      
Key:

R = Resistant.
VR = Variable Resistance depending on temperature and concentration.
NR = Non-resistant.


Chemical Reactivity of Tantalum

ReagentRVRNRReagentRVRNR
Acetic AcidX  Methyl Sulfuric AcidX  
Acetic AnhydrideX  Nickel ChlorideX  
Aluminum ChlorideX  Nickel SulfateX  
Aluminum SulfateX  Nitric AcidX  
Ammonia X Nitric Acid, fumingX  
Ammonium ChlorideX  Nitric OxidesX  
Ammonium Hydroxide X Nitrous AcidX  
Ammonium NitrateX  Nitrosyl ChlorideX  
Ammonium PhosphateX  Organic ChlorideX  
Ammonium SulfateX  Oxalic AcidX  
Amyl Acetate or ChlorideX  Perchloric AcidX  
Aqua RegiaX  PhenolX  
Arsenic AcidX  Phosphoric Acid <4ppmFX  
Barium HydroxideX  Pickling Acids1X  
Bromine, dry (<200°C)X  Phthalic AnyhydrideX  
Calcium HydroxideX  Potassium Carbonate X 
Calcium HypochloriteX  Potassium ChlorideX  
Chlorinated BrineX  Potassium DichromateX  
Chlor. HydrocarbonsX  Potassium Hydroxide2 X 
Chlorine, dry (<175°C)X  Potassium Hydroxide3  X
Chlorine, wetX  Potassium Iodide-IodineX  
Chlorine OxidesX  Silver NitrateX  
Chloracetic AcidX  Sodium Bisulfate, molten  X
Chromic AcidX  Sodium Bisulfate, solutionX  
Chrome Plating SolutionsX  Sodium BromideX  
Cleaning SolutionX  Sodium Carbonate X 
Copper SaltsX  Sodium ChlorateX  
Ethylene DibromideX  Sodium ChlorideX  
Ethyl ChlorideX  Sodium Hydroxide2 X 
Fatty AcidsX  Sodium Hydroxide3  X
Ferric ChlorideX  Sodium HypochloriteX  
Ferric SulfateX  Sodium NitrateX  
Ferrous SulfateX  Sodium SulfateX  
Flourine  XSodium Sulfide X 
Formic AcidX  Sodium SulfiteX  
Fuming Nitric AcidX  Stannic ChlorideX  
Fuming Sulfuric Acid  XSulfur (<500°C)X  
Hydrobromic AcidX  Sulfur DioxideX  
Hydrochloric AcidX  Sulfur Trioxide  X
Hydrocyanic AcidX  Sulfuric Acid (>160°C)X  
Hydrofluoric Acid  XZinc ChlorideX  
Hydrogen BromideX  Zinc SulfateX  
Hydrogen ChlorideX  
Liquid Metals
Hydrogen IodideX  Bismuth (<900°C)X  
Hydrogen PeroxideX  Gallium (<450°C)X  
Hydrogen SulfideX  Lead (<1000°C)X  
Hypochlorous AcidX  Lithium (<1000°C)X  
Iodine (<1000°C)X  Magnesium (<1150°C)X  
Lactic AcidX  Mercury (<600°C)X  
Magnesium ChlorideX  Sodium (<1000°C)X  
Magnesium SulfateX  Sodium - Potassium Alloys (<1000°C)X  
Mercuric ChlorideX  Zinc (<500°C)X  
Notes:Key:
1. Except HNO3-HF.
2. Dilute.
3. Concentrated.
R = Resistant.
VR = Variable Resistance depending on temperature and concentration.
NR = Non-resistant.


Comparative Machinability Ratings of Some Refractory Metals and Other Difficult Materials

 Carbide Tool Machinability Ratings
Workpiece MaterialHardnessSurface Speed (ft/min)Cut Depth (in.)Feed (in/rev)TypeLife (in3)Removal Rate (in3/min)Relative Removal RateRelative Removal Cost
Steel
4130200 BHN4450.120.019C658211.50100.01
413054RC900.120.004C6190.625.419
Superalloys
Rene 41320 BHN700.060.009C2230.474.125
Rene 41365 BHN700.060.009C2160.474.125
Refractory Metals
TZM217 BHN3500.060.009C2992.3020.05
Niobium112 BHN3000.120.005C21512.2019.06
Unalloyed, Wrought Molybdenum223 BHN2750.100.010C11323.3029.04
Note:
Ratings based on metal removal rate for 4130 steel at 100,000 psi tensile strength as 100; lower numbers indicates poorer machinability.


Vacuum Furnaces

In the cold wall vacuum furnace design, heating is from within the vacuum vessel so the heat losses from the work area to the cold wall must be reduced. To be compatible with the vacuum system, the insulation must meet certain requirements. These include:

Molybdenum is an ideal material for this application. Rembar stocks all the materials normally used in vacuum furnaces and can do much of the fabrication of both new and replacement parts.

There are three basic insulation systems that will meet most of the above requirements. These systems can be classified as:

The shield pack insulation system is composed of a multi-layer design that is made up of metal sheets that are separated to form a series of reflective shields. The selection of shield material is dependent on the maximum use-temperature of the system. Most commonly used is molybdenum.

The advantage of Radiant Molybdenum Shielding over other materials is:


Radiant Shield Data for Molybdenum

Heat Shields
Furnace Temperature, x F183218322012201224002400
Cold Shell Temperature, x F100100100100100100
Number of Shields (1 - 10)121212
Avg. Shield Emissivity Factor (0 - 1.0)0.600.600.600.600.600.60
Cold Shell Emissivity Factor (.9 typ)0.900.900.900.900.900.90
 
Computed Shield Temperature IN x F
#1 Shield148416461637181119652167
#2 Shield 1250 1384 1672
 
Computed Heat Loss (KW/ft2)4.02.45.53.39.85.9
 
Furnace Temperature, x F240024002400240021922192
Cold Shell Temperature, x F150150150150100100
Number of Shields (1 - 10)345612
Avg. Shield Emissivity Factor (0 - 1.0)0.600.600.600.600.600.60
Cold Shell Emissivity Factor (.9 typ)0.700.700.700.700.900.90
 
Computed Shield Temperature IN x F
#1 Shield224722822305232017891976
#2 Shield1976208721512194 1517
#3 Shield1563183219662047  
#4 Shield 144417231869  
#5 Shield  13541636  
#6 Shield   1282  
 
Computed Heat Loss (KW/ft2)4.03.12.62.27.34.3

Machining and Welding Nickel-Iron Alloys

(ASTM F-15 and Similar Alloys)

In general, these alloys are not difficult to machine, provided it is noted that these materials work-harden readily. Also note that adequate care is taken on the choice of such factors as tool geometry and material, speeds, feeds, cutting fluids, etc. The following data is intended as a guide to proper selection of these parameters for machining Ni-Fe alloys.

General Machining

Cutting Fluids

A large amount of heat is generated in cutting this material. Consequently, machining is made easier by using a good cutting fluid.

For general machine work, a copious flow (approximately 1 gpm/HP used) of soluble oil is recommended. A chlorinated oil is suggested for use on automatic and semi-automatic machines where a neat oil is required.

Turning and Boring

The general set up for these operations is similar to that used for steel. The following principle should be adhered to as closely as possible.

The following tool geometry, speed and feed values are given as a general guide for use with tungsten carbide tools. The speed and feed figures should generally be reduced by approximately 30% for high-speed steel tools.

DetailRoughing
Value
Finishing
Value
Back rake angle10°
Side rake angle
Front cutting edge
clearance angle
Slide cutting edge
clearance angle
Plan trail angle
Plan approach angle*15°20°
Nose radius0.30 in
(0.8 mm)
0.05 in
(1.3 mm)

Speed and
Feeds
RoughingFinishing
Depth of cut0.1 in
(2.5 mm)
<=0.010 in
(0.25 mm)
Feed (in-mm/rev)0.015 in
(0.4 mm)
>=0.004 in
(0.10 mm)
Speed (SFPM)90120

*Where it is impossible or impractical to apply this value, a decrease in plan approach angle should be followed by an increase in side rake and a decrease in back rake.
Note that the secondary front cutting edge clearance angle should be to suit application.

Planing Techniques

To enable only a light cut to be taken with the finishing tool, roughing cuts should be taken to within approximately 0.25 in. (0.635 mm) of the finished dimension.

A goose neck type of planer tool is recommended for smoother finishing cuts since its shape enables it to withstand the greater mechanical shock encountered when machining Ni-Fe alloys.

The following tool angles are given as a general guide for use with high-speed tools.

DetailRoughing
Value
Finishing
Value
Back rake angle10°-15°
Side rake angle15°
Front cutting edge
clearange angle
Slide cutting edge
clearance angle
Nose radius0.125 in
(3 mm)
0.250 in
(6 mm)
Drilling

The following principles should be observed when drilling Ni-Fe alloys:

Precision Grinding

The methods for grinding Ni-Fe alloys are similar to those used with steel. However, certain conditions require that a slightly softer grade of wheel be used to prevent loading the wheel. A copious flow of lubricant should be used.

Where high permeability is required, final grinding (after annealing) should finish with approximately five cuts progressively decreasing from 0.002 in (0.05 mm) to 0.0002 in (0.005 mm).

Melting Points of Metals

High Medium Low
 °C°F °C°F °C°F
Tungsten34106170Rhodium19663571Neodymium10241875
Rhenium31805756Chromium19303506Silver9611762
Tantalum29965425Zirconium18573375Germanium9471737
Osmium27004892Thorium18453353Lanthanum9201688
Molybdenum26104730Platinum17733223Barium8501562
Iridium24544449Titanium17253137Calcium8481558
Ruthenium24504442Vanadium17103110Cerium8151499
Niobium24684379Palladium15492820Arsenic8141497
Boron23004172Iron15352795Strontium7741425
Hafnium22304046Cobalt14952723Aluminum6601220
Yttrium14902714Magnesium6511204
Nickel14552651Antimony6301166
Erbium14502642Tellurium452846
Beryllium12782332Zinc419786
Manganese12202228Lead327621
Europium11502102Cadmium321610
Uranium11332071Thallium302576
Copper10831981Bismuth271520
Samarium10721962Tin232450
Gold10631945Selenium217423
Silicon14102570Lithium179354
Indium156313
Sodium98208
Potassium62144
Gallium308
Mercury-38.8-38

Densities of Metals

High Medium Low
 G/CC G/CC G/CC
Osmium22.48Bismuth9.90Gallium5.97
Iridium22.42Erbium9.16Arsenic5.73
Platinum21.45Copper8.96Germainium5.32
Rhenium21.02Cobalt8.92Europium5.24
Gold19.30Nickel8.90Selenium4.81
Tungsten19.30Cadmium8.65Titanium4.50
Uranium19.05Niobium8.57Yttrium4.34
Tantalum16.60Iron7.87Barium3.50
Mercury13.55Manganese7.44Aluminum2.70
Hafnium13.09Indium7.31Strontium2.60
Rhodium12.44Tin7.30Boron2.34
Ruthenium12.20Chromium7.14Silicon2.32
Palladium12.02Zinc7.14Beryllium1.84
Thallium11.85Neodynium7.00Magnesium1.74
Thorium11.70Samarium6.93Calcium1.55
Lead11.34Cerium6.78Sodium0.97
Silver10.49Antimony6.68Potassium0.86
Molybdenum10.20Zirconium6.50Lithium0.53
Tellurium6.24
Lanthanum6.19
Vanadium6.11

Brazing Filler Metals

for Refractory Metals

Liquidus Temperature
Brazing Filler Metal°F°C
Ag1760960
Cu19801052
Ni26501454
Pd-Mo28601571
Pt-Mo32251774
Ag-Cu-Mo1435779
Ni-Cu24601349
Mo-Ru34501899
Pd-Cu22001204
Au-Cu1625885
Au-Ni1740949

| Molybdenum | Tungsten | Tantalum | Titanium | Rhenium | Niobium |

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