Inconel Pipe

INCONEL® alloy 718 (UNS N07718/W.Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. Typical composition limits are shown in Table 1. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. The ease and economy with which INCONEL alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.

Chemical Composition , %
Nickel (plus Cobalt) .......................................................50.00-55.00 Chromium......................................................................17.00-21.00
Iron ...............................................................................Balance*
Niobium (plus Tantalum)....................................................4.75-5.50
Molybdenum .....................................................................2.80-3.30 Titanium.............................................................................0.65-1.15
Aluminum ..........................................................................0.20-0.80
Cobalt ...............................................................................1.00 max. Carbon..............................................................................0.08 max.
Manganese .......................................................................0.35 max.
Silicon ...............................................................................0.35 max. Phosphorus.....................................................................0.015 max. Sulfur...............................................................................0.015 max.
Boron ..............................................................................0.006 max. Copper..............................................................................0.30 max 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.              
 

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL® alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic termperatures. Composition is shown in Table 1. The economics of INCONEL alloy X-750 coupled with its availability in all standard mill forms has resulted in applications in a wide variety of industrial fields. In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL alloy X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL alloy X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL alloy X-750 is used from sub-zero to 1200°F. Depending on the application and the properties desired, various heat treatments are employed. For service above 1100°F, particularly where loads are to be sustained for long times, optimum properties are achieved by solution treating (2100°F) plus stabilization treating (1550°F) plus precipitation treating (1300°F). For service below 1100°F, the alloy may be strengthened by precipitation treating after hot or cold working or by precipitation treating after equalizing or solution treating. A furnace-cooling treatment is also used to develop optimum properties for some applications.

Chemical Composition, %
Nickel (plus Cobalt)....................................................70.00 min. Chromium...................................................................14.0-17.0 Iron..................................................................................5.0-9.0 Titanium.......................................................................2.25-2.75 Aluminum....................................................................0.40-1.00
Niobium (plus Tantalum)..............................................0.70-1.20 Manganese.................................................................1.00 max. Silicon.........................................................................0.50 max. Sulfur...........................................................................0.01 max. Copper........................................................................0.50 max. Carbon........................................................................0.08 max.
Cobalt1 .........................................................................1.00 max 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

INCOLOY® alloy 945 (UNS N09945) is a high-strength, corrosion-resistant alloy designed for demanding applications in the oil and gas industry. The properties of this age hardenable nickel-iron-chromium alloy are enhanced by its contents of molybdenum, copper, niobium, titanium, and aluminum. The chemical composition of alloy 945 is seen in Table 1. The alloy’s nickel content results in resistance to chlorideinduced stress corrosion cracking. Nickel, in conjunction with the molybdenum and copper, also gives alloy 945 outstanding resistance to general corrosion in reducing media. Molybdenum also imparts resistance to localized attack (pitting and crevice corrosion). The alloy’s content of chromium provides resistance in oxidizing environments. Niobium, titanium and aluminum participate in the age hardening reaction that occurs during heat treatment. Their interaction forms gamma prime and gamma double prime precipitates, which strengthen the alloy. INCOLOY alloy 945 is suitable for downhole oil and gas applications requiring high strength and corrosion resistance in aggressive sour wells containing high levels of hydrogen sulfide and chorides. Because of the alloy’s resistance to stress cracking in environments rich in hydrogen sulfide, it is suitable for downhole and surface gas-well components including tubular products, valves, hangers, landing nipples, tool joints and packers. The alloy can also be used for fasteners, pump shafting and high strength piping systems. 

Chemical Composition of INCOLOY alloy 945, wt %
Nickel ......…………………………………..…..45.0-55.0
Chromium ..…………………………………….19.5-23.0
Iron ……………….………………………………Balance      
Molybdenum …….………………………………..3.0-4.0
Niobium .…………………………………………..2.5-4.5    
Copper …………………………………………….1.5-3.0
Titanium ….………………………………………..0.5-2.5    
Aluminum ….…………………………………….0.01-0.7
Manganese ...……………………………………1.0 max.  
Silicon …..………………………………………..0.5 max.
Sulfur …..……………………………………….0.03 max.    
Phosphorous .………………………………….0.03 max.
Carbon …..…………………………………0.005 to 0.04 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
       .AVAILABLE IN STOCK.              

Additional Information:

• Minimum Order Quantity: 10 kgs

INCOLOY® alloy 925 (UNS N09925) is an agehardenable nickel-iron-chromium alloy with additions of molybdenum, copper, titanium and aluminum. The alloy’s chemical composition, listed in Table 1, is designed to provide a combination of high strength and excellent corrosion resistance. The nickel content is sufficient for protection against chloride-ion stresscorrosion cracking. The nickel, in conjunction with the molybdenum and copper, also gives outstanding resistance to reducing chemicals. The molybdenum aids resistance to pitting and crevice corrosion. The alloy’s chromium content provides resistance to oxidizing environments. The titanium and aluminum additions cause a strengthening reaction during heat treatment. INCOLOY alloy 925 is used in various applications requiring a combination of high strength and corrosion resistance. Because of the alloy’s resistance to sulfide stress cracking and stress-corrosion cracking in “sour” (H2S containing) crude oil and natural gas, it is used for down-hole and surface gaswell components including tubular products, valves, hangers, landing nipples, tool joints and packers. The alloy is also useful for fasteners, marine and pump shafting and high-strength piping systems.

Chemical Composition (UNS N09925) of INCOLOY alloy 925, % Nickel...........................................................................42.0-46.0
Chromium ....................................................................19.5-22.5 Iron...................................................................................22 min
Molybdenum ....................................................................2.5-3.5 Copper.............................................................................1.5-3.0
Titanium ...........................................................................1.9-2.4 Aluminum.........................................................................0.1-0.5
Manganese ...................................................................1.0 max.
Silicon ...........................................................................0.5 max. Niobium.........................................................................0.5 max.
Carbon ........................................................................0.03 max.
Sulfur ..........................................................................0.03 max.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL® nickel-chromium alloy 625 (UNS N06625/W.Nr. 2.4856) is used for its high strength, excellent fabricability (including joining), and outstanding corrosion resistance. Service temperatures range from cryogenic to 1800°F (982°C). Composition is shown in Table 1. Strength of INCONEL alloy 625 is derived from the stiffening effect of molybdenum and niobium on its nickel-chromium matrix; thus precipitationhardening treatments are not required.The properties of INCONEL alloy 625 that make it an excellent choice for sea-water applications are freedom from local attack (pitting and crevice corrosion), high corrosion-fatigue strength, high tensile strength, and resistance to chloride-ion stress-corrosion cracking. It is used as wire rope for mooring cables, propeller blades for motor patrol gunboats, submarine auxiliary propulsion motors, submarine quickdisconnect fittings, exhaust ducts for Navy utility boats, sheathing for undersea communication cables, submarine transducer controls, and steam-line bellows. Potential applications are springs, seals, bellows for submerged controls, electrical cable connectors, fasteners, flexure devices, and oceanographic instrument components.  

Chemical Composition, %
Nickel…………………………………………….…………58.0 min.
Chromium………………………………………..…………20.0-23.0
Iron………………………………………………..………….5.0 max.
Molybdenum……………………………….……...………8.0-10.0
Niobium (plus Tantalum)…………………..……….3.15-4.15
Carbon……………………………………………..……….0.10 max.
Manganese………………………………………...……….0.50 max.
Silicon……………………………….…………...…………0.50 max.
Phosphorus……………………………………….………..0.015 max.
Sulfur…………………………………..……….…..……..0.015 max. Aluminum…………………………………………………..0.40 max.
Titanium……………………………….……………………0.40 max.
Cobalta ……………………………………………………….1.0 max. 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL® (nickel-chromium-iron) alloy 600 (UNS N06600/W.Nr. 2.4816) is a standard engineering material for applications which require resistance to corrosion and heat. The alloy also has excellent mechanical properties and presents the desirable combination of high strength and good workability. The limiting chemical composition of INCONEL alloy 600 is shown in Table 1. The high nickel content gives the alloy resistance to corrosion by many organic and inorganic compounds and also makes it virtually immune to chloride-ion stress-corrosion cracking. Chromium confers resistance to sulfur compounds and also provides resistance to oxidizing conditions at high temperatures or in corrosive solutions. The alloy is not precipitation hardenable; it is hardened and strengthened only by cold work. The versatility of INCONEL alloy 600 has led to its use in a variety of applications involving temperatures from cryogenic to above 2000°F (1095°C). The alloy is used extensively in the chemical industry for its strength and corrosion resistance. Applications include heaters, stills, bubble towers and condensers for processing of fatty acids; evaporator tubes, tube sheets and flaking trays for the manufacture of sodium sulfide; and equipment for handling abietic acid in the manufacture of paper pulp. The alloy's strength and oxidation resistance at high temperatures make it useful for many applications in the heat-treating industry. It is used for retorts, muffles, roller hearths and other furnace components and for heat-treating baskets and trays. In the aeronautical field, INCONEL alloy 600 is used for a variety of engine and airframe components which must withstand high temperatures. Examples are lockwire, exhaust liners and turbine seals. INCONEL alloy 600 is used in the electronic field for such parts as cathode-ray tube spiders, thyratron grids, tube support members and springs. The alloy is a standard material of construction for nuclear reactors. It has excellent resistance to corrosion by high-purity water, and no indication of chloride-ion stress-corrosion cracking in reactor water systems has been detected. For nuclear applications, the alloy is produced to exacting specifications and is designated INCONEL alloy 600T.

Chemical Composition, %
Nickel (plus Cobalt)....................................................72.0 min. Chromium..................................................................14.0-17.0
Iron ..........................................................................6.00-10.00
Carbon ......................................................................0.15 max.
Manganese ................................................................1.00 max Sulfur.......................................................................0.015 max.
Silicon .......................................................................0.50 max. Copper......................................................................0.50 max.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

NIMONIC® alloy 901 (UNS N09901/W.Nr. 2.4662) is an age-hardenable Ni-Fe-Cr superalloy with significant additions of molybdenum, titanium and aluminum. The alloying route for this highperformance material may include combinations of vacuum induction melting, vacuum arc remelting and electroslag remelting, according to the final application and the customer’s specification. Typically, the alloy is used for gas turbine engine discs, shafts, rings, casings and seals with a maximum service temperature of around 600°C (1100°F). Table 1 - Nominal

Chemical Composition, % (not for specification purposes) Nickel...................................................................................42.5
Chromium ............................................................................12.5 Molybdenum........................................................................5.75 Titanium.................................................................................2.9
Cobalt ...........................................................................1.0 max. Copper..........................................................................0.5 max.
Manganese ...................................................................0.5 max.
Silicon ...........................................................................0.4 max. Aluminum....................................................................0.35 max. Carbon..........................................................................0.1 max.
Sulfur ..........................................................................0.03 max.
Iron ...............................................................................Balance* 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .

SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL™ 713C: FORGING FACTS & CHARACTERISTICS

Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.

CHEMICAL COMPOSITION OF INCONEL™ 713C

• Carbon 0.20
• Manganese 1.0 max
• Sulfur 0.015 max
• Silicon 1.0 max
• Chromium 11.0-14.0
• Molybdenum 3.5-5.5
• Titanium 0.25-1.25
• Aluminum 5.5-6.5
• Iron 5.0 max
• Columbium + Ta 1.0-3.0
• Nickel remainder

APPLICATIONS OF INCONEL™ 713C

• Inconel 713C is most commonly used for jet engine gas turbine blades.

MACHINABILITY OF INCONEL™ 713C

• Machine with single–point cemented tungsten-cobalt grade and tungsten-tantalum-cobalt grade tools or
• High-speed tungsten-cobalt or molybdenum-tungsten-vanadium tools
• Cutting lubricants:
  • Chlorinated, sulfurized  fatty mineral oil
  • Rich emulsion of 10 parts water and 1 part soluble oil
• Surface and cylindrical grind with wheels:
  • Aluminum oxide
  • Vitrified bond of medium or soft hardness and medium open structure
  • Use 1 pound of sal soda with 25 gallons of water, or chemically active grinding coolant

WELDABILTIY OF INCONEL™ 713C

• Inconel 713C can be used in applications using very low restraint
• Use Inco-Weld A electrode
• Flash-butt weld
• Inconel 713C is also good for hydrogen-atmosphere brazing with normal high-heat brazing alloy with electroplated mating surfaces

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.              

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL® alloy 617 (UNS N06617/W.Nr. 2.4663a) is a solid-solution, strengthened, nickel-chromium-cobaltmolybdenum alloy with an exceptional combination of high-temperature strength and oxidation resistance. The alloy also has excellent resistance to a wide range of corrosive environments, and it is readily formed and welded by conventional techniques. The limiting chemical composition of INCONEL alloy 617 is listed in Table 1. The high nickel and chromium contents make the alloy resistant to a variety of both reducing and oxidizing media. The aluminum, in conjunction with the chromium, provides oxidation resistance at high temperatures. Solid-solution strengthening is imparted by the cobalt and molybdenum. The combination of high strength and oxidation resistance at temperatures over 1800°F (980°C) makes INCONEL alloy 617 an attractive material for such components as ducting, combustion cans, and transition liners in both aircraft and land-based gas turbines. Because of its resistance to high-temperature corrosion, the alloy is used for catalyst-grid supports in the production of nitric acid, for heat-treating baskets, and for reduction boats in the refining of molybdenum. INCONEL alloy 617 also offers attractive properties for components of power-generating plants, both fossilfueled and nuclear

CHEMICAL PROPERTIES %
Nickel...........................................................................44.5 min. Chromium....................................................................20.0-24.0 Cobalt..........................................................................10.0-15.0
Molybdenum .................................................................8.0-10.0
Aluminum ........................................................................0.8-1.5
Carbon ........................................................................0.05-0.15 Iron................................................................................3.0 max.
Manganese ...................................................................1.0 max.
Silicon ...........................................................................1.0 max.
Sulfur ........................................................................0.015 max.
Titanium ........................................................................0.6 max. Copper..........................................................................0.5 max.
Boron ........................................................................0.006 max. 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Additional Information:

• Minimum Order Quantity: 10 kgs

INCONEL® alloy 690 (UNS N06690/W. Nr. 2.4642) is a high-chromium nickel alloy having excellent resistance to many corrosive aqueous media and hightemperature atmospheres. In addition to its corrosion resistance, alloy 690 has high strength, good metallurgical stability, and favorable fabrication characteristics. The chemical composition of INCONEL alloy 690 is listed in Table 1. The substantial chromium content gives the alloy outstanding resistance to oxidizing chemicals and to high-temperature oxidizing gases. The high level of nickel imparts resistance to stresscorrosion cracking in chloride-containing environments as well as to sodium hydroxide solutions. The properties of INCONEL alloy 690 are useful for various applications involving nitric or nitric/hydrofluoric acid solutions. Examples are tail-gas reheaters used in nitric acid production and heating coils and tanks for nitric/hydrofluoric solutions used in pickling of stainless steels and reprocessing of nuclear fuels. The alloy’s resistance to sulfur-containing gases makes it an attractive material for such applications as coal-gasification units, burners and ducts for processing sulfuric acid, furnaces for petrochemical processing, recuperators, incinerators, and glass vitrification equipment for radioactive waste disposal. In various types of high-temperature water, alloy 690 displays low corrosion rates and excellent resistance to stress-corrosion cracking. Thus, alloy 690 is widely used for steam generator tubes, baffles, tubesheets, and hardware in nuclear power generation.

CHEMICAL COMPOSITION %
Nickel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58.0 min.
Chromium. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27.0-31.0
Iron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.0-11.0
Carbon. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.05 max.
Silicon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.50 max.
Manganese . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.50 max.
Sulfur . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.015 max.
Copper. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.50 max 

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.               

Inconel 718 (UNS N07718/W.Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. Typical composition limits are shown in Table 1. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. The ease and economy with which Inconel 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.

Chemical Composition of Inconel 718 %

Nickel (plus Cobalt) .....................................50.00-55.00 Chromium...................................................17.00-21.00
Iron ...........................................................Balance*
Niobium (plus Tantalum)................................4.75-5.50
Molybdenum ................................................2.80-3.30 Titanium.......................................................0.65-1.15
Aluminum .....................................................0.20-0.80
Cobalt ..........................................................1.00 max. Carbon...........................................................0.08 max.
Manganese .....................................................0.35 max.
Silicon ...........................................................0.35 max. Phosphorus......................................................0.015 max. Sulfur.............................................................0.015 max.
Boron ............................................................0.006 max. Copper............................................................0.30 max.

Inconel 718

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

.AVAILABLE IN STOCK.

Additional Information:

• Minimum Order Quantity: 10 No(s)

Features

Forgings : ASME SB-564, AMS 5887

Round Bar : ASME SB-166, AMS 5887

Sheet/Plate : ASME SB-168, AMS 5888 ,AMS 5889

INCONEL® alloy 617 (UNS N06617/W.Nr. 2.4663a) is a solid-solution, strengthened, nickel-chromium-cobaltmolybdenum alloy with an exceptional combination of high-temperature strength and oxidation resistance. The alloy also has excellent resistance to a wide range of corrosive environments, and it is readily formed and welded by conventional techniques. The limiting chemical composition of INCONEL alloy 617 is listed in Table 1. The high nickel and chromium contents make the alloy resistant to a variety of both reducing and oxidizing media. The aluminum, in conjunction with the chromium, provides oxidation resistance at high temperatures. Solid-solution strengthening is imparted by the cobalt and molybdenum. The combination of high strength and oxidation resistance at temperatures over 1800°F (980°C) makes INCONEL alloy 617 an attractive material for such components as ducting, combustion cans, and transition liners in both aircraft and land-based gas turbines. Because of its resistance to high-temperature corrosion, the alloy is used for catalyst-grid supports in the production of nitric acid, for heat-treating baskets, and for reduction boats in the refining of molybdenum. INCONEL alloy 617 also offers attractive properties for components of power-generating plants, both fossilfueled and nuclear.

Chemical properties %
Nickel...........................................................................44.5 min. Chromium....................................................................20.0-24.0 Cobalt..........................................................................10.0-15.0
Molybdenum .................................................................8.0-10.0
Aluminum ........................................................................0.8-1.5
Carbon ........................................................................0.05-0.15 Iron................................................................................3.0 max.
Manganese ...................................................................1.0 max.
Silicon ...........................................................................1.0 max.
Sulfur ........................................................................0.015 max.
Titanium ........................................................................0.6 max. Copper..........................................................................0.5 max.
Boron ........................................................................0.006 max.

SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.

       .AVAILABLE IN STOCK.              

 

Additional Information:

• Minimum Order Quantity: 10 Kilogram