Complex Nickel Alloys

Properties: High Temperature Alloys, Heat Resistant, Corrosion Resistant, Creep Resistant
Applications: Aero Engine Parts

	Ni	Cr	Co	Mo	W	Fe	Al	Ti	Cu	Nb	Others
C242	56	21.5	10	10.5	-	0.75*	0.2*	0.3*	-	-	-
C263	50	20	20	5.9	-	0.75*	0.5	2.2	-	-	-
C1023	56	15.5	9.5	8	-	0.25	4.3	3.6	-	-	-
Incoloy 903	38	1.0*	15	-	-	BAL	0.7	1	-	3	-
Incoloy 907	38	1.0*	13	-	-	BAL	0.1	1.5	-	4.7	-
Inconel 617	54	22	12.5	9	-	-	1	-	-	-	0.07 C
Inconel 700	45	15	29	3	-	4	3.3	2.25	-	-	-
IN 100 (PK24)	60	10	15	3	-	-	5.5	4.7	-	-	1.0 V 0.06 Zr
IN-731	66	9.5	10	2.5	-	0.5	5.5	4.65	-	-	0.95 V
IN-738	61	16	8.5	1.75	2.6	0.5	3.4	3.4	-	0.9	1.75 Ta
IN-792	61	12.7	9	2	3.9	-	3.2	4.2	-	-	4.2 Ta 1.0 Hf
IN939 (Nimocast 739)	48	22.4	19	-	2	-	1.9	3.7	-	1	1.4 Ta
Incoloy 807	40	20	8	-	5	26	-	-	-	1	-
SRR99	65	8.6	5	-	9.5	0.1*	5.5	2.2	-	-	2.8 Ta
Nimonic 90	57	20	16	-	-	5.0*	1.5	2.5	-	-	-
Nimonic 91	47.5	28.5	20	-	-	-	1.2	2.3	-	-	-
Nimonic 105/108	53	15	20	5	-	1.0*	4.7	1.2	-	-	-
Nimonic 115/118	57	15	15	3.5	-	1.0*	5	4	-	-	-
Nimonic PK31	49	20	14	4.5	-	1	0.4	2.3	-	5	-
Nimonic PK33	56	19	14	7	-	0.5	2	2	-	-	-
GTD 111	59	14	9.5	1.5	3.8	0.5*	3	4.9	-	-	2.8 Ta 0.02* B
GTD 222	50	22.5	19	-	2	0.25*	1.2	2.3	-	0.8	1.0 Ta
RA 333	45	25	3.5	3.5	3.5	18	-	-	0.5	-	-
Rene 41	52	19	11	10	-	5.0*	1.6	3.2	-	-	-
M252	54	19	10	10	-	5.0*	1	2.6	-	-	-
Thetalloy (PWA 651)	49	25	12.5	3	7	3	-	-	-	-	-
Waspaloy	56	19	14	4.2	-	1.5*	1.4	3	-	-	0.1 Zr
Astraloy	56	15	15	5.25	-	0.2*	4.4	3.5	-	-	0.03 B
Udimet 500 (PK25)	53	17.5	16.5	4	-	4.0*	2.9	3.9	-	-	0.01 B
Udimet 520	56	19	12	6	1	1	2	3	-	-	-
Udimet 600	52	17.5	16.5	4	-	4.0*	4.2	2.9	-	-	0.04* B
Udimet 700 (Rene 77)	52	15	15	4	-	0.5*	4.2	3.5	-	-	0.02* B
Udimet 710	53	18	15	3	1.5	0.5*	2.5	5	-	-	0.035 B
Udimet 720	53	18	15	3	1.4	0.5*	2.5	5	-	-	0.045 B
MAR M-246	60	9	10	2.5	10	0.15	5.5	1.5	-	-	1.5 Ta
Rene 80	60	14	9.5	4	4	-	3	5	-	-	-
Rene 88	55	16	13	4	4	0.25	2.1	3.75	-	0.7	0.02* B
B1900 (PWA 663)	64	8	10	6	-	-	6	1	-	-	1.0 Zr 4.0 Ta
B1914	66	10	10	3	-	-	5.5	5.3	-	-	0.1 B
B1925	61	12	8.5	1.8	4.5	-	3.5	4	-	-	0.1 B 4.0 Ta
B1950 (MAR M-200)	60	9	10	-	12	-	5	2	-	1	0.12 B
B1964	59	9	10	1	8.5	-	3.5	5.3	-	-	0.16 B 2.5 Ta
MAR M-002	59	10	10	-	10	1.0*	5	1.5	-	-	2.5 Ta 1.5 Hf
MAR M-247	58	8.5	10	0.6	10	0.5*	5.5	1	-	-	3.0 Ta 1.5 Hf
MARAGING 200	18	-	8.5	3.2	-	BAL	-	0.20	-	-	0.03* C
MARAGING 250	18	-	8	5	-	BAL	-	0.40	-	-	0.03* C
MARAGING 300	18.5	-	9	5	-	BAL	-	0.65	-	-	0.03* C
MARAGING 350	18	-	11.5	5	-	BAL	-	1.35	-	-	0.03* C

* indicates maximum

R.E.M. Aerospace cannot accept responsibility for any errors or omissions that may have occurred during its compilation.