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Ensinger PEI

ATI Wah Chang Nb/Nb Alloy C-103
Categories: Metal; Nonferrous Metal; Niobium Alloy

Material Notes: This alloy satisfies most rocket engine applications for temperatures up to 2700°F because of superior mechanical properties at all temperatures. Offers weight savings over many rocket engine design materials.

Information provided by ATI Wah Chang

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Physical PropertiesMetricEnglishComments
Density 8.86 g/cc0.320 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate  65.5 MPa
@Temperature 1480 °C
9500 psi
@Temperature 2700 °F
Vacuum
 89.6 MPa
@Temperature 1370 °C
13000 psi
@Temperature 2500 °F
Vacuum
 186 MPa
@Temperature 1090 °C
27000 psi
@Temperature 2000 °F
Vacuum
 310 MPa
@Temperature 871 °C
45000 psi
@Temperature 1600 °F
Vacuum
 310 MPa
@Temperature 538 °C
45000 psi
@Temperature 1000 °F
Vacuum
 317 MPa
@Temperature 649 °C
46000 psi
@Temperature 1200 °F
Vacuum
 321 MPa
@Temperature 760 °C
46500 psi
@Temperature 1400 °F
Vacuum
 421 MPa
@Temperature 23.0 °C
61000 psi
@Temperature 73.4 °F
Tensile Strength, Yield  59.3 MPa
@Temperature 1480 °C
8600 psi
@Temperature 2700 °F
Vacuum
 72.4 MPa
@Temperature 1370 °C
10500 psi
@Temperature 2500 °F
Vacuum
 138 MPa
@Temperature 1090 °C
20000 psi
@Temperature 2000 °F
Vacuum
 162 MPa
@Temperature 871 °C
23500 psi
@Temperature 1600 °F
Vacuum
 172 MPa
@Temperature 760 °C
25000 psi
@Temperature 1400 °F
Vacuum
 186 MPa
@Temperature 649 °C
27000 psi
@Temperature 1200 °F
Vacuum
 200 MPa
@Temperature 538 °C
29000 psi
@Temperature 1000 °F
Vacuum
 296 MPa
@Temperature 23.0 °C
43000 psi
@Temperature 73.4 °F
Elongation at Break  15 - 17 %
@Temperature 649 °C
15 - 17 %
@Temperature 1200 °F
Vacuum
 16 - 18 %
@Temperature 760 °C
16 - 18 %
@Temperature 1400 °F
Vacuum
 18 - 19 %
@Temperature 871 °C
18 - 19 %
@Temperature 1600 °F
Vacuum
 19 - 21 %
@Temperature 538 °C
19 - 21 %
@Temperature 1000 °F
Vacuum
 25 - 30 %
@Temperature 23.0 °C
25 - 30 %
@Temperature 73.4 °F
 >= 45 %
@Temperature 1090 °C
>= 45 %
@Temperature 2000 °F
Vacuum
 >= 70 %
@Temperature 1370 °C
>= 70 %
@Temperature 2500 °F
Vacuum
 >= 70 %
@Temperature 1480 °C
>= 70 %
@Temperature 2700 °F
Vacuum
Modulus of Elasticity 90.0 GPa13100 ksi
 64.0 GPa
@Temperature 1200 °C
9280 ksi
@Temperature 2190 °F
Charpy Impact  107 J
@Temperature -73.3 °C
79.0 ft-lb
@Temperature -100 °F
Notched
 201 J
@Temperature 23.0 °C
148 ft-lb
@Temperature 73.4 °F
 
Thermal PropertiesMetricEnglishComments
CTE, linear  6.84 µm/m-°C
@Temperature 93.3 °C
3.80 µin/in-°F
@Temperature 200 °F
 7.02 µm/m-°C
@Temperature 316 °C
3.90 µin/in-°F
@Temperature 600 °F
 7.20 µm/m-°C
@Temperature 538 °C
4.00 µin/in-°F
@Temperature 1000 °F
 7.38 µm/m-°C
@Temperature 760 °C
4.10 µin/in-°F
@Temperature 1400 °F
 7.74 µm/m-°C
@Temperature 982 °C
4.30 µin/in-°F
@Temperature 1800 °F
 8.10 µm/m-°C
@Temperature 1200 °C
4.50 µin/in-°F
@Temperature 2200 °F
Thermal Conductivity  38.0 W/m-K
@Temperature 871 °C
264 BTU-in/hr-ft²-°F
@Temperature 1600 °F
 40.6 W/m-K
@Temperature 1113 °C
282 BTU-in/hr-ft²-°F
@Temperature 2035 °F
 44.61 W/m-K
@Temperature 1300 °C
309.6 BTU-in/hr-ft²-°F
@Temperature 2380 °F
Melting Point 2300 - 2400 °C4170 - 4350 °F
Solidus 2300 °C4170 °F
Liquidus 2400 °C4350 °F
Maximum Service Temperature, Air 1480 °C2700 °Fmost rocket engine applications
 
Optical PropertiesMetricEnglishComments
Emissivity (0-1)  0.28
@Temperature 800 °C
0.28
@Temperature 1470 °F
Total Hemispherical
 0.40
@Temperature 1200 °C
0.40
@Temperature 2190 °F
Total Hemispherical
 0.87
@Temperature 37.8 °C
0.87
@Temperature 100 °F
Cycle 3
 0.89
@Temperature 1320 °C
0.89
@Temperature 2400 °F
Cycle 3
 0.89
@Temperature 37.8 °C
0.89
@Temperature 100 °F
Cycle 2
 0.89
@Temperature 37.8 °C
0.89
@Temperature 100 °F
Cycle 1
 0.92
@Temperature 1320 °C
0.92
@Temperature 2400 °F
Cycle 1
 0.92
@Temperature 1320 °C
0.92
@Temperature 2400 °F
Cycle 2
 
Component Elements PropertiesMetricEnglishComments
Hafnium, Hf 10 %10 %
Niobium, Nb (Columbium, Cb) 87 - 87.6 %87 - 87.6 %as balance
Tantalum, Ta 0.50 %0.50 %
Titanium, Ti 0.70 - 1.3 %0.70 - 1.3 %
Tungsten, W 0.50 %0.50 %
Zirconium, Zr 0.70 %0.70 %
 
Descriptive Properties
Enthalpy, BTU/lb1031610°F
 1452017°F
 1842390°F

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

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