RA 602 CA - Rolled Alloys

DATA SHEET
Features
• Outstanding resistance to cyclic
oxidation through 2250°F (1232°C)
• Excellent high temperature creeprupture
strength
• Resistant to carburizing environments
• Highly resistant to grain growth in
service
• Superior behavior in oxidizing/
chloridizing environments
• Good resistance to metal dusting
Applications
• Calciners shells
• Muffles and retorts
• Chemical vapor deposition retorts
• Nitric acid catalyst support grids
• Radiant tubes
• Vacuum furnace fixtures
• Molten glass process equipment
• Vitrification of nuclear wastes
• Reheaters & convection tubes in direct
reduction iron ore (DRI) plants
Chemical Composition Range, %
Min Max
Chromium 24.0 26.0
Nickel balance
Carbon 0.15 0.25
Aluminum 1.8 2.4
Titanium 0.1 0.2
Yttrium 0.05 0.12
Zirconium 0.01 0.10
Manganese -- 0.15
Silicon -- 0.5
Copper -- 0.1
Iron 8.0 11.0
Specifications
UNS N06025 W.Nr. 2.4633
ASTM B 168/ASME SB168
Plate, Sheet, Strip
ASTM B 166/ASME SB166
Rod, Bar, Wire
Weld Wire: ERNiCrFe-12
Covered electrodes: ENiCrFe-12
ASME Code Case 2359 to 1800°F (1032°C)
Stress, psi
1
RA 602 CA
RA 602 CA ®
ALLOY
Performance Profile
RA 602 CA provides some of the best combined high
temperature properties of any nickel alloy available.
RA 602 CA is one of the most oxidation resistant nickel
alloys. A high chromium content, along with aluminum
and yttrium additions, permits the alloy to develop a
tightly adherent oxide scale. A relatively high carbon
content combined with titanium and zirconium additions
results in high creep rupture strength.
RA 602 CA may be considered for applications where
it is important to minimize product contamination while
maintaining high mechanical integrity at extreme
temperatures.
10000
1000
RA600
Haynes ® 230
RA 353 MA
RA333 ®
RA 601
RA 602 CA
2200°F Cyclic Oxidation Testing
3040 Hours Cycled Weekly
0 100 200 300 400 500
Weight Gain (mg/cm 2 )
Average 10,000 Hour Rupture Strength 3,4,5
Haynes
230
RA330
RA602CA
100
1200 1400 1600 1800 2000 2200
Temperature, °F

RA 602 CA
2100°F (1149°C) Cyclic Oxidation Testing 1,2
3000 Hours Cycled Weekly
RA330 ®
RA 353 MA ®
RA333 ®
Alloy 617
Haynes ® 230
RA 602 CA
Oxidation Resistance
0 10 20 30 40 50 60
Weight Gain (mg/cm 2 )
RA 602 CA is one of the most oxidation resistant nickel
alloys available. Outstanding oxidation resistance is
achieved through a high chromium content (25%)
supplemented with aluminum (2.2%) and a
microalloying addition (0.1%) yttrium. High chromium
contents are known to be beneficial for resisting
oxidation. The aluminum addition allows for the
formation of a continuous homogenous self repairing
AI 2 O 3 subscale. The addition of yttrium improves the
adhesion and spalling resistance of the chromium and
aluminum oxide scales. The extremely low scaling rate
of RA 602 CA makes it an excellent candidate for
RA 602 CA after 3150 hours exposure to
2100°F (1149°C) Magnification: 200x
RA 601
H
Haynes ® 214
2
Alloy 617
RA 353 MA
RA333 ®
RA 602 CA
2250°F Cyclic Oxidation Testing
3000 Hours Cycled Weekly
0 100 200 300 400 500
Weight Gain (mg/cm 2 )
applications such as calciners, where minimal
contamination from scaling is permissible.
The figures below compare the appearance of
RA 602 CA versus RA601 after more than 3000 hours
at 2100°F (1149°C). RA601, as seen, has extensive
internal oxidation attack6 . In contrast, only a thin surface
oxide scale formed on RA 602 CA2 . This is especially
important in applications that use thin sheet such as
radiant tubes. No internal oxidation means the entire
wall thickness is sound metal and the alloy retains a
greater amount of its original properties.
RA601 after 3150 hours exposure to
2100°F (1149°C) Magnification: 200x

Grain Growth
The brittle fracture of components exposed to
extreme temperatures is a common occurrence.
At temperatures near or exceeding the annealing
temperature of a heat resistant alloy, grain growth is
likely to occur. Extensive grain growth can result in a
loss of ductility. As a result, the component can be
prone to brittle fracture. An alloy 601 corrugated muffle
that suffered brittle fracture due to combination of
extensive grain growth and carburization is shown
above.
The results of testing at 2050°F (1121°C) are detailed
in the table below. The information provides a
comparison of various heat resisting alloys that are
commonly used above 1900°F (1038°C). The data was
compiled from intermittent exposure of sample
coupons to 2050°F (1121°C) for a total of 990 hours.
Each sample was in the mill annealed condition. The
figure at right shows a sample of RA 602 CA after long
term exposure to 2100°F (1149°C).
3
RA 602 CA
Brittle fracture of an alloy 601 muffle from the combination of extensive grain growth and carburization.
Sample of RA 602 CA examined after exposure to
2100°F (1149°C) for over 3150 hours. The grain size
was originally ASTM 7. After the 3000 hour test
period the grains had only grown to ASTM 5.5.
Magnification: 90x
Effects of High Temperature Exposure on ASTM Grain Size8 - 2050°F (1121°C)
Time ASTM Average Grain Size
Hours RA 602 CA RA601 601GC RA330 RA 353 MA RA333 RA600
0 7 5 5.5 7 6 4 8
2 7 5 5.5 3.5 4 4 4
24 7 1.5 5 3.5 3 3.5 1
72 7 1 5 3 2.5 3 0
184 6.5 1 3.5 3 2.5 2.5 0
344 6.5 0 3.5 2.5 2 2 0
510 6.5 0 3 2 2 2 00
670 6.5 00 3 2 1.5 2 00
830 6.5 00 3 2 1.5 2 00
990 6.5 00 2.5 1.5 1.5 1 00

RA 602 CA
Carburization 8
Extended exposure to methane (CH 4 ), carbon
monoxide (CO), and other carbon rich gases can lead
to carburization. As heat resistant alloys absorb carbon,
their ductility will gradually decrease. Alloys that are
high in nickel, such as RA 602 CA possess excellent
Metal Wastage Rate (mg/cm 2 h)
1.00E-01
1.00E-02
1.00E-03
1.00E-04
1.00E-05
1.00E-06
RA600
0 2000 4000 6000 8000 10000
Exposure Time (Hours)
4
resistance to carburization attack. RA 602 CA forms a
tenacious oxide scale, which provides increased
protection from carburization. This protective scale
impedes the carbon fro being absorbed into the base
metal.
Cyclic Carburization in CH /H Environment (A =0.8), Weight Change (mg/m 4 2 c 2h) 850°C (1562°F) 1000°C (1832°F) 1150°C (2102°F)
RA310 130 305 —
RA800AT 143 339 813
RA600 50 190 626
RA601 64 170 508
RA 602 CA 13 70 175
Metal dusting is a form of carburization that can lead
to the rapid corrosion of heat resistant alloys. The
photo at left shows a section of an RA330 fan shroud
taken from a carburizing furnace displaying the pitting
typical of metal dusting attack.
The combination of high aluminum and chromium
additions to RA 602 CA results in a resistance to metal
dusting superior to alloys such as RA330, RA600,
RA601, and 800HT ® alloy.
RA601
RA 602 CA
Coupon testing
of alloys in
simulated metal
dusting
atmosphere
consisting of
H 2 +CO+H 2 O at
650°C (1202°F).

Hot Corrosion 9
Weight change values for
nickel alloys exposed for 100
hours at 800°C (1472 °F)
Weight Gain (mg/cm2)
Physical Properties Melting Range: 2350-2550°F (1288-1400°C)
Permeability at 20°C/68°F (RT):

RA 602 CA
Mechanical Properties
Typical Tensile Properties, Solution Treated 2228°F (1220°C)
Temperature, °F Tensile Strength, psi 0.2% Yield Strength, psi Elongation, % Reduction of Area, %
68 105,000 50,500 38 39
800 95,400 39,200 42 33
900 94,600 38,600 43 35
1000 93,400 38,300 40 36
1200 84,000 37,700 48 45
1400 54,400 36,500 55 52
1500 41,200 34,800 78 72
1600 32,800 28,700 82 72
1700 24,900 21,000 82 74
1800 17,100 15,200 78 75
1900 13,600 12,200 80 72
2000 13,000 11,600 85 74
2100 10,200 9,000 86 78
2200 5,800 5,000 96 76
Note: Above 1155°F (624°C), time dependent properties, ie., creep-rupture are the basis for design.
Typical Tensile Properties (Metric)
Temperature, °C Tensile Strength, MPa 0.2% Yield Strength, MPa Elongation, % Reduction of Area, %
20 721 348 38 39
400 664 272 42 32
600 632 262 36 37
800 311 251 76 74
900 198 180 82 72
1100 789 78 86 75
1200 42 39 92 76
ASME Allowable Stresses (Code Case 2359-1)
For Metal Maximum For Metal Maximum
Temperature Not Allowable Temperature Not Allowable
Exceeding, °F Stress Values Exceeding, °F Stress Values
ksi {Notes (1) ksi {Notes (1)
and (2)} and (2)}
100 26.0 1100 9.2
200 25.5 1150 6.9
300 24.7 1200 4.1
400 23.7 1250 2.8
500 22.7 1300 2.0
600 21.7 1350 1.5
650 21.2 1400 1.2
700 20.8 1450 0.97
750 20.5 1500 0.80
800 20.2 1550 0.68
850 20.0 1600 0.58
900 19.8 1650 0.51
950 19.6 1700 0.44 (Note 3)
1000 16.3 1750 0.37 (Note 3)
1050 12.3 1800 0.32 (Note 3)
General Note: Time Dependent Values are shown in italics
6
Please consult Code Case 2359-1 for all
requirements for designing with RA 602
CA to Section 1 and Section VIII, Division
1 requirements.
Notes:
(1) This alloy in the solution-annealed
condition is subject to severe loss of
rupture ductility in the temperature range
of 1200-1400°F.
(2) The allowable stress values are based
on the revised criterion for tensile strength
of 3.5, where applicable.
(3) For Section VIII, Division 1 use only.
(4) The criteria used to establish allowable
stresses at design temperatures above
1500°F included consideration of the Favg factor as defined in Appendix 1 of Section
II, Part D.
(5) Creep-fatigue, thermal ratcheting, and
environmental effects are increasingly
significant failure modes at temperatures
in excess of 1500°F and shall be
considered in the design.

Creep-Rupture Properties 3
RA 602 CA possesses excellent creep rupture
properties. The relatively high carbon level in the alloy
ensures the precipitation of bulky homogeneously
distributed carbides. Alloying with titanium and
zirconium ensures that these carbides and also
carbonitrides are finely distributed. Even solution
annealing at 1200°C (2192°F) does not completely
7
RA 602 CA
dissolve these carbides. As a result, the alloy achieves
its high creep strength through a combination of solid
solution hardening and carbide strengthening.
RA 602 CA has a strength advantage over RA601 at
all temperatures. At temperatures in the 1800-1900°F
(982-1038°C) range and above, RA 602 CA has
equivalent or greater creep rupture properties than
Haynes 230 alloy.
Creep-Rupture Properties, grain size 70 µm or coarser ( ≅ ASTM 4.5 or coarser)
Temperature Average Stress to Rupture, psi Average Stress for 1% Total Creep, psi
°F 1,000 Hrs 10,000 Hrs 100,000 Hrs 1000 Hrs 10,000 Hrs 100,000 Hrs
1200 37,700 31,200 20,300 31,900 26,800 20,900
1400 17,400 11,300 5800 13,900 9400 5400
1600 4600 3200 1750 3500 2380 1300
1700 3600 2180 1100 2230 1520 910
1800 2300 1490 740 1300 960 580
1900 1700 990 485 810 590 320
2000 1250 670 (310) 540 330 (160)
2100 670 440 (200) 260 140 (60)
Temperature Average Stress to Rupture, MPa Average Stress for 1% Total Creep, MPa
°C 1,000 Hrs 10,000 Hrs 100,000 Hrs 1,000 Hrs 10,000 Hrs 100,000 Hrs
650 260 215 140 220 185 120
700 155 100 132 85
750 90 48 75 46
800 42 20 32 16.5
850 26 14 19 9.7
900 18 9.7 2.2 13 7.5
950 13 6.7 8.8 5.4
1000 14.1 9.0 4.5 7.5 5.8 3.4
1050 6.2 3.1 3.6 1.9
1100 7.2 4.4 (2.1) 3.2 1.9 0.85
1150 3.0 (1.4) 1.0 0.40
1200 3.0 1.9 (0.42) 0.97

RA 602 CA
Fatigue Properties10 Fatigue strength of
RA 602 CA at elevated
temperatures.
Impact Properties 9
Loading ± σ m ,N/mm2
100
80
60
40
20
1100°C
1000°C
Effects of Long Term Exposure at Elevated Temperatures on Ductility 3
0
1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07
Number of Cycles
Condition Aging Temperature Time at Aging Impact Strength
°C (°F) Temperature Joules (ft-lb)
Annealed N/A 0 78-84 (58-62)
Annealed 500°C (932°F) 8000 30 (22.1)
Annealed 640°C (1184°F) 8000 30 (22.1)
Annealed 740°C (1364°F) 8000 27 (20)
Annealed 840°C (1544°F) 8000 58 (42.8)
10% Cold Worked 500°C (932°F) 8000 22 (16.2)
10% Cold Worked 640°C (1184°F) 8000 27 (20)
10% Cold Worked 740°C (1364°F) 8000 25 (18.4)
10% Cold Worked 840°C (1544°F) 8000 68 (50.2)
10% C.W. + Aged + Annealed 500°C (932°F) 8000 78 (58)
10% C.W. + Aged + Annealed 640°C (1184°F) 8000 85 (62.7)
10% C.W. + Aged + Annealed 740°C (1364°F) 8000 76 (56.1)
10% C.W. + Aged + Annealed 840°C (1544°F) 8000 80 (59)
8
1150°C

Forming
Hot Working
RA 602 CA may be hot-worked in the temperature
range 1200 to 900°C (2190 to 1650°F), followed by
water quenching or rapid air cool. As with other
austenitic alloys, do not attempt to form in the 600-
800°C (1100-1500°F) temperature range.
Heating must be performed in a furnace with accurate
temperature control, and a neutral to slightly oxidizing
atmosphere. The atmosphere should not fluctuate
between oxidizing and reducing. Natural gas used to
fire the furnace should contain no more than 0.1
weight % sulfur, and fuel oil no more than 0.5% sulfur.
Spin formed radiant tube return bend. 6 inch
diameter on 6 inch centers formed out of 11ga
(0.120”) RA 602 CA sheet.
Heat Treatment
RA 602 CA is solution annealed at 2160-2230°F
(1180-1220°C) followed by water quenching. For
sheet 16 gage (1.5mm) and lighter, rapid air cooling
is acceptable.
9
RA 602 CA
The flame must not impinge directly on the workpiece.
Do not heat RA 602 CA, or any other nickel alloy,
with a torch to bend it. The lack of temperature control
will often result in cracking.
Cold Forming
RA 602 CA has a high carbon content, and work
hardens rapidly. RA 602 CA may be bent 120° around
a diameter equal to three times the material thickness
(3T bend) for material up to 0.4” (10 mm) thick. This
grade cannot be bent to as tight a radius as the lower
carbon alloys, e.g, RA600 or RA330.
As with other nickel alloys, the shear drag (burr)
should be removed, or placed on the inside of the
bend. During bending this heavily cold-worked burr
may initiate cracking. Sawed plate may be preferred
for severe forming operations.
3/8” thick retort head press formed from 3/8” thick
RA 602 CA plate. 3-1/2 inch deep and 17 inches in
diameter.

RA 602 CA
Welding
GTAW - Gas Tungsten Arc Welding
10,000 Hour Creep Rupture
Strength, N/mm2
30
25
20
15
RA 602 CA Base Metal
10
-18%
RA 602 CA GTAW
5
W/Matching Filler
-16%
0
800 900 1000
-16%
1100
-18%
1200
Temperature, °C
10.000 hour stress to rupture values of RA 602 CA
GTAW weld as compared to RA 602 CA base metal. 10
RA 602 CA may be joined by Gas Tungsten Arc
Welding and by Plasma Arc Welding. In both cases
the back side of the weld root must be shielded with
100% welding grade argon (not nitrogen). Good root
shielding is required because of the high aluminum
content of this alloy. The torch gas must be 97.5%
argon, 2.5% nitrogen, for both processes. The
2.5% N 2 addition to the argon is necessary for
improved weldability and reduced hot cracking
susceptiblity in RA 602 CA.
Manual GTAW Parameters
Shielding gas: 98% Argon - 2% Nitrogen
Plate Filler Metal Root Pass Filler Pass Travel Arc Energy Shielding
Thickness Diameter Speed Gas Flow
inches inches Amps Volts Amps Volts in/min KJ/in, max cfh
11 ga 0.063 90-100 11 -- -- 4-6 20 17-21
1/4 0.063-0.094 110 11 130-150 15 4-6 20 17-21
1/2 0.094 110 11 130-150 15 4-6 20 17-21
Automatic GTAW Parameters
Shielding gas: 98% Argon - 2% Nitrogen
Plate Filler Metal Root Pass Filler Pass Travel Arc Energy Shielding
Thickness Diameter Speed Gas Flow
inches inches Amps Volts Amps Volts in/min KJ/in, max cfh
11 ga 0.035-0.045 manual 150-250 10-15 8-12 20 30-40
5/16 0.035-0.045 manual 150-250 10-15 8-12 20 30-40
10
Stress, psi
45,000
40,000
35,000
UTS Base Metal
YS Base Metal
UTS Weld
30,000
25,000
20,000
15,000
10,000
5,000
0
YS Weld
1500 1600 1700 1800 1900 2000 2100 2200
Temperature, °F
Comparison of mechanical properties of RA 602 CA
base metal vs. GTAW welds made with matching
filler.
Interpass temperature should not exceed 250°F
(120°C) with lower temperatures preferred. Heat the
metal before welding only if necessary to dry the
workpiece, and then just hot to the touch. Neither
preheat nor postheat is required.
The matching weld filler wire is S 6025, W.Nr. 2.4649,
AWS ERNiCrFe-12.

GMAW - Gas Metal Arc Welding
11
RA 602 CA
GMAW welding of RA 602 CA should be performed using the matching composition weld wire designated as
S 6025. RA 602 CA should be joined using the pulse arc process. For welding material thicknesses less than
3/16” thick use of 100% Argon shielding has been satisfactory. For welding thicknesses above 3/16”, it is recommended
to utilize the welding gas AR Ni5He5CD300. (Available from Airgas 419-666-7155) to reduce the
likelihood of centerline cracking.
GMAW – Pulse Arc Transfer
Wire Diameter Wire Feed Amperes Volts Gas Flow Travel Speed Pulse
0.045 inch 236 in/min 170 A 26 V 38 ft 3 /hr 15 in/min 500 pulse/sec
For applications under 1832°F (1000°C), RA 602 CA may be welded with alloy 617 wire, ERNiCrCoMo-1, using
argon or argon-helium shielding gas. A GTAW cover pass with S 6025 filler wire is necessary to match the
oxidation resistance of the RA 602 CA base metal. S 6025 weld filler should be used at higher temperatures
where alloy 617 has less strength than RA 602 CA base metal.
SMAW - Shielded Metal Arc Welding
Matching chemistry DC basic covered electrodes, 6225 Al (AWS ENiCrFe-12), are available for welding
RA 602 CA. Use a stringer bead technique, electrode inclined approximately 20° in the direction of travel. Keep
the interpass temperature low, below 300°F (150°C). Electrodes must be dry. If necessary, rebake to dry for 2
hours at 480°F (250°C).
6225 Al Electrode Weld Deposit 8 - Nominal Chemical Composition, %
Cr Ni C AI Ti Y Zr Mn Si Fe
25 62 0.2 1.8 0.1 0.02 0.03 0.1 0.6 10
SMAW Weld Metal Mechanical Properties, Room Temperature (minimum)
Ultimate Tensile 0.2% Yield Strength Elongation Impact Strength
Strength
psi N/mm 2 psi N/mm 2 % Ft-lb J
101,500 700 72,500 500 15 22 30
Starting Parameters
Electrode diameter, inch (mm) 3/32 (2.5) 1/8 (3.2) 3/16 (4.0)
DCRP Current, Amps 40-55 70-90 90-110

RA 602 CA
PAW - Plasma Arc Welding
As with automatic GTAW, shielding gas must be Argon with 2-3% Nitrogen
Plate Filler Metal Root Pass Filler Pass Travel Arc Energy Shielding
Thickness Diameter Speed Gas Flow
inches inches Amps Volts Amps Volts in/min KJ/in, max cfh
3/16 0.045 180 25 -- -- 10-12 28 65
1/2 0.045 180 25 GMAW 10-12 28 65
Dissimilar Welding
RA 602 CA may be welded to carbon steel, 304 stainless steel, or RA600 using ERNiCr-3 (Alloy 82) bare wire or
ENiCrFe-3 (Alloy 182) covered electrodes.
Joints between RA 602 CA and RA601 may be made using the matching RA 602 CA weld filler, Nicrofer S 6025.
Weldments to other heat resistant or nickel alloys should be qualified before production. Choice of weld filler
should be based on high temperature service properties, in addition to weldability considerations.
Corrosion Rate, mm/a
0.2
0
-0.2
-0.4
-0.6
RA 602 CA GTAW SMAW
Base Metal
1100°C 1200°C
Comparison of the oxidation of RA 602 CA base metal to GTAW and SMAW welds
made with matching ERNiCrFe-12 and ENiCrFe-12 filler metal respectively.
12

25” O.D. calciner processing metal oxide pigments
in the 1800-2100°F range. RA 602 CA selected after
coupon testing of RA601, HR-120, Haynes 556, and
HR-160 alloys. Reference RA Case History #2027.
60 inch diameter x 30 ft. long calciner processing
high purity alumina at 2050-2100°F. Unit in operation
for 5 years until first repairs. RA 602 CA selected
over alloy 601 based on higher strength and scaling
resistance.
Serpentine grid formed from 3/16" RA 602 CA plate.
Material used in vacuum heat treatment of tool
steels at 2175°F-2275°F followed by 6 bar nitrogen
quench. Still in service after 1200 cycles. See Case
History 2063.
13
RA 602 CA
Furnace rolls in a specialty steel mill. RA 602 CA
replaced water cooled asbestos lined carbon steel.
The RA 602 CA is not water cooled and was rolled
and welded to form the rolls. RA 602 CA rolls have
reduced energy consumption by eliminating watercooling
and have reduced marking of sheet product
due to their smooth surface.
30” diameter chemical vapor deposition (CVD)
retort for the aluminide coating of gas turbine
blades. RA 602 CA replaced Haynes 230 in this
application. Temperatures are 1975°F.

RA 602 CA
Radiant tube formed out of 11 ga RA 602 CA sheet.
Replaced type HT cast tubes. RA 602 CA tubes
preferred due to their lighter weight, which translates
into easier installation and greater furnace efficiency.
Tube still in service after 18 months no distortion
reported. Reference RA Case History 2026.
Test of RA 602 CA vs. alloy 600 belly bands on an
aluminide coating retort. 69 cycles of operation at
2000°F. RA 602 CA is now specified for this application
over alloy 600. See Bulletin 2032 for more details.
14
RA 602 CA liner being formed prior to welding.
Liner is replacing alloy 800HT ® in a hydrogen
reformer bypass duct. Metal dusting has historically
been a problem with the alloy 800HT liners.
RA 602 CA coating cans fabricated from 11ga
sheet. RA 602 CA replaced Haynes 214 ® alloy. Due
to the light gage and temperatures in the 1900-
2000°F range oxidation resistance is critical in this
application.

15
RA 602 CA

RA 602 CA
References
1. J.C. Kelly & J. D. Wilson, “Oxidation Rates of Some Heat Resistant
Alloys”, ASM Proceedings of the 2nd International Conference on
Heat-Resistant Materials, Gatlinburg, TN, USA. September 11-14,
1995.
2. Rolled Alloys Laboratory Testing, Investigation File #99-55.
3. Personal Correspondence with Krupp VDM 9/28/00.
4. Rolled Alloys, Inc. RA Data Sheet, RA330 Alloy, Bulletin 107, 9/98.
5. Haynes International, Haynes 230 Alloy Data Sheet, H-3000F, pgs
5, 6.
6. Rolled Alloys Laboratory Testing, Investigation File #92-99.
7. Rolled Alloys Laboratory Testing, Investigation File #00-05.
8. D.C. Agarwal & U. Brill, & J. Kloewer, “Recent Results on Metal
Dusting of Nickel Based Alloys and Some Applications,” Corrosion
2001, Paper 1382, NACE International, Houston TX 2001.
9. R. Bender & M. Schultze, “Oxidation Beharior of Several
Commercial Alloys in Chlorine Containing High Temperature
Environments.
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Form
# 1602
6/
04
500
10. ThyssenKrupp VDM, VDM Report No. 25, High-Temperature Alloys
from Krupp VDM for Industrial Engineering.
11. D.C. Agarwal & U. Brill “Performance of Alloy 602CA (UNS N06025)
in High Temperature Environments up to 1200�C”, Corrosion/2000,
Paper 521, NACE International, Orlando, FL 2000.
General Disclaimer
The data and information in this data sheet are believed to be
reliable, however, this data is not intended as a substitute for competent
professional engineering assistance which is a requisite to any
specific application.
Trade Marks:
602 CA is a registered trademark of ThyssenKrupp VDM.
RA330 and RA333 are registered trademarks of Rolled Alloys, Inc.
Haynes 230 and Haynes 214 are registerd trademarks of Haynes
International.
RA 353 MA is a registered trademark of Outokumpu Stainless.
800HT is a registered trademark of Special Metals.
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Rolled Alloys
Voorerf 16
4824 GN Breda, The Netherlands
+31-(0)76-548 44 44 fax +31-(0)76-542 98 88
email:sales@rolledalloys.nl
INTERNATIONAL:
Rolled Alloys International, Ltd.
14, The Oaks
Clews Road, Redditch, Worcestershire
B98 7ST, United Kingdom
+44-(0)1527-401101 fax +44-(0)1527-401013
email:hbuijnsters@rolledalloys.co.uk
SINGAPORE:
Rolled Alloys International, Ltd. Singapore
10 Anson Road #24-06
International Plaza, Singapore 079903
+65-62272725 fax +65-62272735
email:railtd@pacific.net.sg
CHINA:
Rolled Alloys, Ltd.
Room 12B03, 12B Floor
Suncome Liauw's Plaza
738 Shangcheng Road, Pudong New Area
Shanghai, China 200120
+86-(0)21-5835-5329 fax +86-(0)21-5835-5339
E-mail: sales@rolledalloys.com
http://www.RolledAlloys.com
© 2016
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Rolled
Alloys,
Inc.
Litho
in
U.
S.
A.