IS 4432:1988 15Ni5Cr4Mo1-S Steel: Specifications & Listings

IS 4432:1988 15Ni5Cr4Mo1-S: 15Ni5Cr4Mo1-S is 15Ni5Cr4Mo1 in IS 4432:1988 ordered with the narrower sulphur range 0.020 to 0.035 percent (clause 5.1, Limit 2); the letter S is added to the grade name. The standard covers wrought low carbon unalloyed and alloy steel bars, billets, rods and finished forgings for case hardening.

Category: Alloy Steel
Grade Details
GradeIS 4432:1988 15Ni5Cr4Mo1-S
Standard IS 4432:1988
ApplicationsForgings and fabrication of case-hardened machine or automobile parts
Equivalent / Similar Grades
Grade Standard Region Live on M-EX
IS 4432 15Ni5Cr4Mo1 IS 4432:1988 India No activity yet
Grade ComparisonCompare With a Specific Grade →
Grade Standard Match
IS 4432 15Ni5Cr4Mo1 IS 4432:1988 Strong Match
EN 10084 17NiCrMoS6-4 EN 10084:2008 Close Alternative
EN 10084 17NiCrMo6-4 EN 10084:2008 Close Alternative
BS 970 (Part 3) 815M17 BS 970 (Part 3):1991 Close Alternative
EN 10084 20NiCrMoS6-4 EN 10084:2008 Close Alternative
BS 970 (Part 1) 815M17 BS 970 (Part 1):1983 Close Alternative
BS 970 (Part 1) 815H17 BS 970 (Part 1):1983 Close Alternative
EN 10084 18CrNiMo7-6 EN 10084:2008 Close Alternative
Matched by chemical composition and mechanical properties, not a formal equivalence claim. Always verify against the applicable standard before substitution.
Chemical Composition (%)
C Si Mn Ni Cr Mo S P
0.12-0.18 0.15-0.35 0.60-1.00 1.00-1.50 0.75-1.25 0.08-0.15 0.020-0.035 <=0.035
Mechanical Properties
Core Tensile Strength 1050-1350 MPa (16 mm) / 1000-1350 MPa (30 mm) / 900-1200 MPa (63 mm)
Core Yield Strength >=720 MPa (16 mm) / >=700 MPa (30 mm) / >=600 MPa (63 mm)
Core Elongation >=8% (16 mm) / >=9% (30 mm) / >=11% (63 mm)
Core Reduction of Area >=35% (16 mm) / >=35% (30 mm) / >=40% (63 mm)
Hardness, annealed (A) <=229 HB

More data from IS 4432:1988

From the standard
Sulphur and phosphorus limits ordering options
Sulphur
0.020 to 0.035 percent
Phosphorus
0.035 percent max
Sulphur in the product, unless otherwise agreed
0.017 percent min
Designation
Letter S added at the end of the grade name
Sulphur and phosphorus range can also be ordered under clause 5.1, Limit 2.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 1 note 1, clause 5.1, Table 2 note 1
Other composition limits from the clauses and notes
Deoxidation
Fully killed, unless otherwise agreed
Elements not specified for this grade, if present, maximum
Cu 0.25, V 0.05 percent
Copper plus 10 times tin, maximum
0.50 percent
Micro-alloying elements
Titanium, niobium, vanadium or boron may be added by agreement, singly or together
Elements not specified in Table 1 are not added except by agreement or to finish the heat. Reasonable precautions are taken against unwanted elements from scrap.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 1 notes, clauses 3, 3.1 and 5.3
Heat treatment temperatures 4 values
Hot working temperature range
1150 to 850 °C
Normalising temperature
840 to 870 °C
Full annealing (A) temperature
860 to 880 °C
Sub-critical anneal for softening, after normalising
650 to 700 °C
Recommended temperatures, for guidance only, for controlling hardness, machinability and shearability.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 3
Case hardening treatment 7 values
Jominy end quench test, quenching temperature
870 ± 5 °C
Carburising temperature
890 to 940 °C
Direct and single hardening temperature
810 to 840 °C
Double hardening, core hardening temperature
840 to 880 °C
Double hardening, case hardening temperature
780 to 820 °C
Quenching medium
Oil / thermal bath / poly quench
Tempering temperature
180 to 220 °C
Recommended conditions for reaching the core properties below, for guidance only. Time for austenitising about 45 minutes for a 25 mm section; tempering at least 1 hour, preferably 90 minutes. For direct and single quenching use fully aluminium killed fine grained steel. If direct hardened, a carburising temperature of 940 °C is generally not exceeded. Thermal bath includes suitable salt baths.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 5
Core properties after case hardening, by test bar diameter 3 sections
Tensile strength (MPa)Yield strength, min (MPa)Elongation, min (%)Reduction of area, min (%)Test bar diameter (mm)
1050 to 135072083516
1000 to 135070093530
900 to 1200600114063
Core properties of simulated case-hardened test bars, treated as in the case hardening treatment above. Values apply to test bars taken from rounds in the direction of rolling. Applies when the steel is ordered on this basis.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 4
Hardness by delivery condition 3 conditions
As rolled (R), maximum
263 HB
Annealed to maximum hardness (A), maximum
229 HB
Treated for improved machinability (M)
170 to 220 HB
Brinell hardness. A different as-rolled maximum for cold shearability, or a different range for improved machinability, may be agreed at the time of order.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 6, clause 7.2
Hardenability, end quench test Hardness band
Hardness band (HRC, minimum to maximum) by distance from the quenched end (mm)
1.5
5
20
30
40
Distance from quenched end (mm)1.55203040
Maximum, HRC4746383530
Minimum, HRC3636262422
Recommended values. Jominy test as per IS 3848. Minor variation in ladle analysis from Table 1 is permitted for steel with guaranteed hardenability.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 7
Blank hardened hardness core strength guarantee
Blank hardened hardness, HRC
35
Blank hardening treatment
870 ± 10 °C, 45 minutes soak, followed by oil quenching
Blank hardening is done on a 30 mm diameter turned specimen from the same location of the billet as the tensile specimen; hardness is taken at the centre. Recommended value, applies when agreed.
Source: IS 4432:1988 with Amendment 1 (April 1994), Table 7 notes 1 and 2, clause 14.1 (d)

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