ZH
RU
ES

double antibody room temperature

double antibody room temperature, Total:384 items.

In the international standard classification, double antibody room temperature involves: Ceramics, Rubber, Plastics, Farming and forestry, Fasteners for aerospace construction, Paints and varnishes, Surface treatment and coating, Protection against fire, Products of the textile industry, Elements of buildings, Construction industry, Farm buildings, structures and installations, Testing of metals, Aircraft and space vehicles in general, Materials for aerospace construction, Fruits. Vegetables, Powder metallurgy, Fasteners, Refractories, General methods of tests and analysis for food products, Coatings and related processes used in aerospace industry, Non-ferrous metals, Conducting materials, Products of non-ferrous metals, Adhesives, Hand-held tools.

American Society for Testing and Materials (ASTM), double antibody room temperature

ASTM C1499-03 Standard Test Method for Monotonic Equibiaxial Flexural Strength of Advanced Ceramics at Ambient Temperature
ASTM C1161-13 Standard Test Method for Flexural Strength of Advanced Ceramics at Ambient Temperature
ASTM F2523-13 Standard Practice for Blowout Resistance of Room-Temperature Vulcanized Elastomers
ASTM C1273-05 Standard Test Method for Tensile Strength of Monolithic Advanced Ceramics at Ambient Temperatures
ASTM C1424-04 Standard Test Method for Monotonic Compressive Strength of Advanced Ceramics at Ambient Temperature
ASTM F2523-07 Standard Practice for Blowout Resistance of Room-Temperature Vulcanized Elastomers
ASTM C1273-05(2010) Standard Test Method for Tensile Strength of Monolithic Advanced Ceramics at Ambient Temperatures
ASTM F2523-05 Standard Practice for Blowout Resistance of Room-Temperature Vulcanized Elastomers
ASTM C1424-15(2019) Standard Test Method for Monotonic Compressive Strength of Advanced Ceramics at Ambient Temperature
ASTM F2523-07e1 Standard Practice for Blowout Resistance of Room-Temperature Vulcanized Elastomers
ASTM C1273-95a(2000) Standard Test Method for Tensile Strength of Monolithic Advanced Ceramics at Ambient Temperatures
ASTM C1424-99 Standard Test Method for Monotonic Compressive Strength of Advanced Ceramics at Ambient Temperatures
ASTM C1469-00 Standard Test Method for Shear Strength of Joints of Advanced Ceramics at Ambient Temperature
ASTM C1469-00(2005) Standard Test Method for Shear Strength of Joints of Advanced Ceramics at Ambient Temperature
ASTM C1469-10 Standard Test Method for Shear Strength of Joints of Advanced Ceramics at Ambient Temperature
ASTM C1684-13 Standard Test Method for Flexural Strength of Advanced Ceramics at Ambient Temperaturemdash;Cylindrical Rod Strength
ASTM C1684-13e1 Standard Test Method for Flexural Strength of Advanced Ceramics at Ambient Temperaturemdash;Cylindrical Rod Strength
ASTM C1468-06 Standard Test Method for Transthickness Tensile Strength of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperature
ASTM C1468-00 Standard Test Method for Transthickness Tensile Strength of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperature
ASTM C1468-13 Standard Test Method for Transthickness Tensile Strength of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperature
ASTM C1360-01 Standard Practice for Constant-Amplitude, Axial, Tension-Tension Cyclic Fatigue of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperatures
ASTM C1360-96 Standard Practice for Constant-Amplitude, Axial, Tension-Tension Cyclic Fatigue of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperatures
ASTM C1360-01(2007) Standard Practice for Constant-Amplitude, Axial, Tension-Tension Cyclic Fatigue of Continuous Fiber-Reinforced Advanced Ceramics at Ambient Temperatures
ASTM C1275-00(2005)e1 Standard Test Method for Monotonic Tensile Behavior of Continuous Fiber-Reinforced Advanced Ceramics with Solid Rectangular Cross-Section Test Specimens at Ambient Temperature
ASTM C1275-10 Standard Test Method for Monotonic Tensile Behavior of Continuous Fiber-Reinforced Advanced Ceramics with Solid Rectangular Cross-Section Test Specimens at Ambient Temperature
ASTM C1358-05 Standard Test Method for Monotonic Compressive Strength Testing of Continuous Fiber-Reinforced Advanced Ceramics with Solid Rectangular Cross-Section Test Specimens at Ambient Temperatures
ASTM C1358-96(2000) Standard Test Method for Monotonic Compressive Strength Testing of Continuous Fiber-Reinforced Advanced Ceramics with Solid Rectangular Cross-Section Specimens at Ambient Temperatures
ASTM C1358-18 Standard Test Method for Monotonic Compressive Strength Testing of Continuous Fiber-Reinforced Advanced Ceramics with Solid Rectangular Cross Section Test Specimens at Ambient Temperatures

Group Standards of the People's Republic of China, double antibody room temperature

T/CSTM 00025-2019 Liquid silicone rubber— Two components cured at ambient

Taiwan Provincial Standard of the People's Republic of China, double antibody room temperature

CNS 13957-1997 Method of test for tensile strength of fine ceramics at room and elevated temperature

SE-SIS, double antibody room temperature

SIS SMS 2958-1972 Vitreous enamels. Determination of resistance to citric acid at room temperature

Standard Association of Australia （SAA）, double antibody room temperature

AS 1391:2005 Metallic materials - Tensile testing at ambient temperature
AS 2313.1.13:2006 Methods of test for single sided and double sided pressure-sensitive adhesive tape - Adhesion - Resistance to shear (holding power) at ambient temperature

Professional Standard - Chemical Industry, double antibody room temperature

HG/T 4221-2011 Dual-component silicone rubber vulcanized at normal temperature for mold-making
HG/T 4221-2001 Two-component room temperature vulcanized silicone mold glue

Inner Mongolia Provincial Standard of the People's Republic of China, double antibody room temperature

DB15/T 936-2015 Technical regulations for the cultivation of Agaricus bisporus in solar greenhouse
DB15/T 2783-2022 Greenhouse Technical Regulations for the Identification of Edible Sunflower Anti-Redang Physiological Races

British Standards Institution (BSI), double antibody room temperature

BS A 320:1997 Nuts, anchor, self-locking, floating, self-aligning, two lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235°C, 900 MPa (at ambient temperature)/315°C, 900 MPa (at ambient temperature)/425°C. Dimensions
BS A 333:1999 Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions
BS ISO 3209:2016 Aerospace. Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 C, 1 100 MPa (at ambient temperature)/315 C and 1 100 MPa (at ambient temperature)/ 425 C.
BS EN 12833:2001 Skylight and conservatory roller shutters - Resistance to snow load - Test method
BS EN ISO 6892-1:2016 Metallic materials. Tensile testing. Method of test at room temperature
BS EN ISO 6892-1:2019 Metallic materials. Tensile testing. Method of test at room temperature
BS EN 2907:1996 Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1 100 MPa (at ambient temperature)/650 °C
BS EN ISO 16282:2008 Methods of test for dense shaped refractory products. Determination of resistance to abrasion at ambient temperature
BS EN 3724:2004 Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength class: 1100 MPa (at ambient temperature)
BS EN 2925:1994 Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A 286). Classification: 900 MPa (at ambient temperature)/650°C
BS EN 3720:1995 Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C
BS EN 2909:1995 Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel FE-PA92HT (A 286), silver plated - Classification: 1100 MPa (at ambient temperature)/650 °C
BS EN 2926:1996 Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 900 MPa (at ambient temperature)/650 °C
DD CEN/TS 843-9:2010 Advanced technical ceramics. Mechanical properties of monolithic ceramics at room temperature - Method of test for edge-chip resistance
BS EN 3012:1996 Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy) - Classification: 1210 MPa (at ambient temperature)/730 °C
BS EN IEC 61788-24:2018 Superconductivity - Critical current measurement. Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires
BS EN 3019:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286) - Classification: 1100 MPa (at ambient temperature)/650 °C
BS EN 4084:2010 Aerospace series. Nuts, anchor, self-locking, fixed, two lug, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) / 235°C
BS EN 2865:2010 Aerospace series. Nuts, anchor, self-locking, floating, two lugs, with counterbore, in heat resisting steel, MoS2 lubricated. Classification: 1100 MPa (at ambient temperature) / 315 C
BS EN 4084:2009 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature) / 235 °C
BS EN 2865:2009 Aerospace series - Nuts, anchor, self-locking, floating, two lugs, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature) / 315 °C
BS ISO 15490:2008 Fine ceramics (advanced ceramics, advanced technical ceramics) - Test method for tensile strength of monolithic ceramics at room temperature
BS EN 3724:2003 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001 MoSDOWN2 coated - Classification: 1 100 MPa (at ambient temperature)
BS EN 3013:1996 Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated - Classification: 1210 MPa (at ambient temperature)/730 °C
BS EN 3843:2010 Aerospace series. Nuts, bihexagonal, self-locking, with counterbore, in heat resisting steel, passivated. Classification: 1100 MPa (at ambient temperature)/650°C
BS EN 2927:1996 Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Classification:1275 MPa (at ambient temperature)/650 °C
BS EN 2680:2006 Nuts, anchor, self-locking, floating, self-aligning, two lug, in alloy steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature) / 235 °C
BS EN 3907:2004 Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1100MPa (at ambient temperature)/350 °C
BS EN 3721:1995 Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel, FE-PA92HT (A 286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C
BS EN 3907:2003 Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoSDOWN2 coated - Classification: 1100 MPa (at ambient temperature)/350 °C
BS EN 3020:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa (at ambient temperature)/650 °C
BS EN 2264:1996 Nuts, anchor, self-locking, floating, two lug, incremental counterbore, in alloy steel, cadmium plated MoS2 lubricated - Classification: 900 MPa (at ambient temperature) /235 °C
BS EN 2869:2010 Aerospace series. Nuts, hexagonal, slotted/castellated, normal height, normal accross flats, in heat resisting steel, passivated. Classification: 1100 MPa (at ambient temperature) / 650°C
BS EN 3834:2010 Aerospace series - Nuts, anchor, self-locking, floating, two lug, incremental counterbore, in corrosion resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C
BS EN 2869:2009 Aerospace series - Nuts, hexagonal, slotted/castellated, normal height, normal accross flats, in heat resisting steel, passivated - Classification: 1100 MPa (at ambient temperature) / 650 °C
BS EN 2930:1996 Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated - Classification:1210 MPa (at ambient temperature)/730 °C
BS EN 4125:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C
BS EN 3435:2010 Aerospace series - Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C
BS ISO 17162:2014 Fine ceramics (advanced ceramics, advanced technical ceramics). Mechanical properties of monolithic ceramics at room temperature. Determination of compressive strength
BS EN 2874:1996 Bolts, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated - Classification: 1550 MPa (at ambient temperature) /315 °C
BS EN 2928:1996 Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated - Classification: 1275 MPa (at ambient temperature)/650 °C
BS EN 2870:1996 Bolts, normal bihexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature) /315 °C
BS EN 2881:2006 Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature) / 120 °C
BS EN 4126:2010 Aerospace series - Nuts, anchor, self-locking, floating, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C
BS ISO 23242:2020 Fine ceramics (advanced ceramics, advanced technical ceramics). Test method for flexural strength of monolithic ceramic thin plates at room temperature by three-point or four-point bending
BS EN 3063:1994 Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification: 1210 MPa (at ambient temperature)/730°C
BS EN 3537:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C
BS EN 658-5:2003 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Determination of interlaminar shear strength by short span bend test (three points)
BS EN 658-5:2002 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Determination of interlaminar shear strength by short span bend test (three points)

European Association of Aerospace Industries, double antibody room temperature

AECMA PREN 3537-1990 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification: 1100 MPa (at Ambient Temperature)/315 Degrees Celsius Edition 1
AECMA PREN 3537-1993 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius Edition P 1; Corrigendum 5/10/93
AECMA PREN 3538-1993 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, Reduced Series, with Counterbore , in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature) / 315 Degrees Celsius Edition P 1; Corrigendum 5/10/1993
AECMA PREN 4009-1994 Aerospace Series Bolts, Double Hexagon Head, Close Tolerance Shank, Medium Length Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Classification : 1 550 MPa (at Ambient Temperature) / 650 Degrees C Edition P1
AECMA PREN 4255-1997 Aerospace Series Nuts, Anchor,Self-Locking, Fixed, Two Lug, with Counterbore, in Heat Resisting Steel, Silver Plated Classification: 1 100 MPa (at Ambient Temperature) / 425 Degrees C Edition P 1
AECMA PREN 4256-1997 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, Reduced Series with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) /425 Degrees C Edition P 1
AECMA PREN 4352-1999 Aerospace Series Bolts, Double Hexagon Head with Lockwire Holes, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-PH2601 (Inconel 718), MoS2 Coated Classification: 1 550 MPa (at Ambient Temperature) / 425 Degrees C Edition P 1
AECMA PREN 4321-1999 Aerospace Series Bolts, Double Hexagon Head with Lockwire Holes, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-PH2601 (Inconel 718), Silver Plated Classification: 1 550 MPa (at Ambient Temperature) / 650 Degrees C Edition P 1
AECMA PREN 4219-1996 Aerospace Series Nuts, Hexagon, Self-Locking by Domed Plastic Cap, Normal Height, Normal Across Flats, in Corrosion Resisting Steel, Passivated Classification : 900 MPa (at Ambient Temperature) / 120 Degrees Celsius Edition P 1
AECMA PREN 4219-1995 Aerospace Series Nuts, Hexagon, Self-Locking by Domed Plastic Cap, Normal Height, Normal Across Flats, in Corrosion Resisting Steel, Passivated Classification : 900 MPa (at Ambient Temperature) / 120 Degrees Celsius Edition P1; Superseding C 3/ WG 5 N 23
AECMA PREN 4117-1993 Aerospace Series Nuts, Bihexagonal, Self- Locking, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718), Silver Plated on Thread Classification : 1 500 MPa (at Ambient Temperature) / 600 Degrees C Edition P1
AECMA PREN 3536-1996 Aerospace Series Nuts, Hexagon, Self-Locking, in Heat Resisting Steel, MoS2 Lubricated Classification: 1 100 MPa (at Ambient Temperature) / 315 Degrees Celsius Edition P 2
AECMA PREN 3435-1993 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, Reduced Series, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification: 1 100 MPa (at Ambient Temperature)/315 Degrees C Edition P 1; Corrigendum
AECMA PREN 2879-1998 Aerospace Series Nuts, Anchor, Self-Locking, Fuel Resistant, Sealing, Floating, Two Lug, With Counterbore, in Corrosion Resisting Steel, Passivated, MoS2 Lubricated Classification: 900 MPa (At Ambient Temperature) / 235 Degrees C Edition P 1
AECMA PREN 2883-1995 Aerospace Series Nuts, Hexagonal, Self-Locking, with Counterbore and Captive Washer, in Heat Resisting Steel, MoS2 Lubricated Classification: 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius Edition P 1
AECMA PREN 3539-1993 Aerospace Series Nuts, Anchor, Self-Locking, One Lug, Fixed, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature) / 315 Degrees Celsius Edition P 1
AECMA PREN 2264-1995 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, Incremental Counterbore, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature)/235 Degrees Celsius Edition 2
AECMA PREN 4013-1993 Aerospace Series Shank Nuts, Self-Locking, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718), Silver Plated Classification: 1 550 MPa (at Ambient Temperature) / 600 Degrees C Edition P1
AECMA PREN 2884-1987 Aerospace Series Bolts, Pan Head, Torq-Setrm Recess, Coarse Tolerance Shank, Short Thread, in Titanium Alloy, Anodised Classification: 1100 MPa/315 Degrees Celsius Issue P 1
AECMA PREN 4069-1994 Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Passivated Classification: 600 MPa (at Ambient Temperature) / 650 Degrees C Edition 1
AECMA PREN 2680-1996 Aerospace Series Nuts, Anchor, Self Locking, Floating, Self- Aligning, Two Lug, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification : 900 MPa (at Ambient Temperature) / 235 Degrees Celsius Issue P 2
AECMA PREN 2680-1998 Aerospace Series Nuts, Anchor, Self Locking, Floating, Self- Aligning, Two Lug, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature) / 235 Degrees Celsius Edition P 3
AECMA PREN 4082-1994 Aerospace Series Screws, Pan Head, Slotted, Threaded to Head, in Heat and Corrosion Resisting Steel, Passivated Classification : 900 MPa (at Ambient Temperature)/650 Degrees C Edition P1
AECMA PREN 4083-1995 Aerospace Series Nuts, Bihexagonal, Self-Locking, Reduced Height, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature) / 315 Degrees Celsius Edition P 1
AECMA PREN 4084-1993 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, with Counterbore, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification: 1 100 MPa (at Ambient Temperature) / 235 Degrees C Edition P1
AECMA PREN 3444-1996 Aerospace Series Bolts, Large Bihexagonal Head, Close Tolerance Normal Shank, Medium Length Thread, in Heat Resisting Nickel Base Alloy, Passivated Classification: 1 250 MPa (at Ambient Temperature) / 650 Degrees C Edition P 1
AECMA PREN 3672-1994 Aerospace Series Shank Nuts, Self-Locking, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy), Silver Plated, for 30 Degree Swage Classification: 1 210 MPa (at Ambient Temperature)/730 Degrees C Edition P 1; Corrigendum
AECMA PREN 4047-1998 Aerospace Series Nuts, Self-Locking, MJ Threads, in Heat Resisting Nickel Base Alloy NI-PH2601 (Inconel 718), Silver Plated Classification: 1 550 MPa (at Ambient Temperature) / 600 Degrees C Technical Specification Edition P1
AECMA PREN 3672-1990 Aerospace Series Shank Nuts, Self Locking, Flange Restrained, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Silver Plated Classification: 1210 MPa/730 Degrees Celsius Edition 1
AECMA PREN 4048-1998 Aerospace Series Nuts, Self-Locking, MJ Threads, in Heat Resisting Nickel Base Alloy NI-PH2601 (Inconel 718), MoS2 Coated Classification: 1 550 MPa (at Ambient Temperature) / 425 Degrees C Technical Specification Edition P1
AECMA PREN 3757-1998 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Self-Aligning, Two Lug, in Heat Resisting Steel, MoS2 Lubricated Classification : 900 MPa (at Ambient Temperature) / 315 Degress C Edition P 2
AECMA PREN 4011-1996 Aerospace Series Nuts, Bihexagonal, Self- Locking, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718), Silver Plated Classification: 1 550 MPa (at Ambient Temperature) / 600 Degrees C Edition P1
AECMA PREN 3757-1993 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Self-Aligning, Two Lug, in Heat Resisting Steel, MoS2 Lubricated Classification : 900 MPa (at Ambient Temperature) / 315 Degress C Edition P 1; Corrigendum 05/10/1993
AECMA PREN 3907-1994 Aerospace Series Bolts, Double Hexagon Head, Normal Shank, Long Thread, in Titanium Alloy TI-P63, MoS2 Coated Classification: 1 100 MPa (at Ambient Temperature)/350 Degrees C Edition P 1
AECMA PREN 4012-1993 Aerospace Series Nuts, Bihexagonal, Self- Locking, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718), MoS2 Coated Classification: 1 550 MPa (at Ambient Temperature) / 425 Degrees C Edition P1
AECMA PREN 4251-1997 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 425 Degrees C Edition P 1
AECMA PREN 4252-1997 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, Reduced Series with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) /425 Degree C Edition P 1
AECMA PREN 4253-1997 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Closed Corner, Reduced Series with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 425 Degrees C Edition P 1
AECMA PREN 4254-1996 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 60 Degree Corner, with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 425 Degrees Celsius Edition P1; Superseding C3 No 2515
AECMA PREN 4254-1997 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 60 Degree Corner, with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 425 Degrees C Edition P 1
AECMA PREN 3714-1989 Aerospace Series Nuts, Anchor, Self-Locking, Two Lug, Floating, with Counterbore, in Heat Resisting Steel, Silver Plated Classification : 1100 MPa (at Ambient Temperature)/425 Degrees C Edition 1
AECMA PREN 3714-1993 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, with Counterbore, in Heat Resisting Steel, Silver Plated Classification: 1 100 MPa (at Ambient Temperature)/425 Degrees C Edition P 1; Corrigendum
AECMA PREN 4390-1997 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Self-Aligning, Two Lug, in Heat Resisting Steel, Silver Plated, Classification : 900 MPa (at Ambient Temperature) / 425 Degrees Celsius Edition P 1
AECMA PREN 2894-1995 Aerospace Series Nuts, Bihexagonal, Self-Locking, with counterbore, in Heat Resisting Nickel Base Alloy, Passivated, MoS2 Lubricated Classification: 1 550 MPa (at Ambient Temperature)/315 Degrees Celsius Edition P 1
AECMA PREN 2894-1992 Aerospace Series Nuts, Bi-Hexagonal, Self-Locking, with Counterbore, in Heat Resisting Nickel Base Alloy, Passivated, MoS2 Lubricated Classification : 1 550 MPa (at Ambient Temperature)/315 Degrees C Edition P 1
AECMA PREN 3720-1991 Aerospace Series Nuts, Bihexagonal, Self-Locking, in Heat Resisting Steel FE-PA92HT (A286), MoS2 Coated Classification: 1100 MPa (at Ambient Temperature)/425 Degrees C Issue P 1
AECMA PREN 4125-1994 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Two Lug, Reduced Series, with Incremental Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature) /315 Degrees C Edition P1
AECMA PREN 4126-1993 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, Reduced Series, with Incremental Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature) / 315 Degrees Celsius Edition P1
AECMA PREN 4591-2000 Aerospace Series Nuts, Barrel, Self-Locking, Floating, Self-Aligning, in Heat Resisting Nickel Base Alloy, MoS2 Lubricated Classification: 1 550 MPa (at Ambient Temperature)/315 Degrees C Edition P 1
AECMA PREN 3832-1992 Aerospace Series Bolts, Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Classification: 1 550 MPa (at Ambient Temperature)/650 Degrees C Edition P 1
AECMA PREN 3721-1991 Aerospace Series Nuts, Bihexagonal, Self-Locking, Deep Counterbored, in Heat Resisting Steel FE-PA92HT (A286), MoS2 Coated Classification: 1100 MPa (at Ambient Temperature)/425 Degrees C Issue P 1
AECMA PREN 3722-1991 Aerospace Series Shank Nuts, Self-Locking, in Heat Resisting Steel FE-PA92HT (A286), MoS2 Coated Classification: 1100 MPa (at Ambient Temperature)/425 Degrees C Issue P 1
AECMA PREN 3723-1991 Aerospace Series Nuts, Hexagonal, Self-Locking, in Heat Resisting Steel FE-PA92HT (A286), MoS2 Coated Classification: 1100 MPa (at Ambient Temperature)/425 Degrees C Issue P 1
AECMA PREN 4126-1994 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, Reduced Series, with Incremental Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature) /315 Degrees C Edition P1
AECMA PREN 4218-1999 Aerospace Series Inserts, Thin Wall, Locked and Self-Locking, MJ Threads, in Heat Resisting Steel, Passivated and MoS2-Lubricated Classification: 1100 MPa (at Ambient Temperature) / 315 Degrees Celsius Technical Specification Edition P1
AECMA PREN 4421-2000 Aerospace Series Studs, in Titanium Alloy TI-P64001, MoS2 Coated, with Serrated Locking Ring in Corrosion Resisting Steel Strength Class: 1 100 MPa (at Ambient Temperature) Edition P 1
AECMA PREN 4322-1998 Aerospace Series Bolts, Double Haxagon Head with Lockwire Holes, Relieved Shank, Long Thread, in Titanium Alloy TI-P63, Anodized, MoS2 Coated Strength Class: 1 100 MPa (at Ambient Temperature) Edition P1
AECMA PREN 4297-1995 Aerospace Series Nuts, Hexagon, Self-Locking by Plastic Ring, Normal Height, Normal Across Flats, in Corrosion Resisting Steel, Passivated Classification : 900 MPa (at Ambient Temperature)/120 Degrees C Edition P 1
AECMA PREN 4297-1996 Aerospace Series Nuts, Hexagon, Self-Locking by Plastic Ring, Normal Height, Normal Across Flats, in Corrosion Resisting Steel, Passivated Classification: 900 MPa (at Ambient Temperature) /120 Degrees C Edition P 1

Jiangxi Provincial Standard of the People's Republic of China, double antibody room temperature

DB36/T 1626-2022 Technical regulations for low temperature and adversity cultivation of double cropping rice

Shanxi Provincial Standard of the People's Republic of China, double antibody room temperature

DB14/T 1156-2015 Technical regulations for cultivation of Agaricus bisporus in solar greenhouse

General Administration of Quality Supervision, Inspection and Quarantine of the People‘s Republic of China, double antibody room temperature

GB/T 42667-2023 Test method for iso-biaxial bending strength of fine ceramics at room temperature Double ring method
GB/T 42472-2023 Critical current measurement of retained critical current after double bending of silver-coated Bi-2223 superconducting wire at room temperature

CEN - European Committee for Standardization, double antibody room temperature

EN ISO 8290:1998 Vitreous and Porcelain Enamels - Determination of Resistance to Sulfuric Acid at Room Temperature

RO-ASRO, double antibody room temperature

STAS 10207/8-1976 VITREOUS ENAMELS Determination of resistance to citric acid at room temperature

International Organization for Standardization (ISO), double antibody room temperature

ISO 8290:1987 Vitreous and porcelain enamels; Determination of resistance to sulfuric acid at room temperature
ISO 6892-1:2009 Metallic materials - Tensile testing - Part 1: Method of test at room temperature
ISO 5014:1997 Dense and insulating shaped refractory products - Determination of modulus of rupture at ambient temperature
ISO 6892-1:2016 Metallic materials - Tensile testing - Part 1: Method of test at room temperature
ISO 15490:2008 Fine ceramics (advanced ceramics, advanced technical ceramics) - Test method for tensile strength of monolithic ceramics at room temperature
ISO 15490:2000 Fine ceramics (advanced ceramics, advanced technical ceramics) - Test method for tensile strength of monolithic ceramics at room temperature
ISO 17162:2014 Fine ceramics (advanced ceramics, advanced technical ceramics) - Mechanical properties of monolithic ceramics at room temperature - Determination of compressive strength

Society of Automotive Engineers (SAE), double antibody room temperature

SAE AMS3731/1-1981 POTTING COMPOUND, EPOXY Bisphenol A-Type Unfilled, Room Temperature Cure
SAE AMS3731/1A-2011 POTTING COMPOUND, EPOXY Bisphenol A-Type Unfilled, Room Temperature Cure
SAE AMS3731/5A-2011 POTTING COMPOUND, EPOXY Bisphenol A-Type Filled, Room Temperature Cure, Low Exotherm
SAE AMS3731/7-1981 POTTING COMPOUND, EPOXY Bisphenol A-Type Filled, Room Temperature Cure, Low Shrinkage
SAE AMS3731/7A-2011 POTTING COMPOUND, EPOXY Bisphenol A-Type Filled, Room Temperature Cure, Low Shrinkage
SAE AMS3731/5-1981 POTTING COMPOUND, EPOXY Bisphenol A-Type Filled, Room Temperature Cure, Low Exotherm
SAE AMS3731/10A-1987 POTTING COMPOUND, EPOXY Bisphenol A-Type Unfilled, Room Temperature Cure, Semiflexible
SAE AMS3731/10-1981 POTTING COMPOUND, EPOXY Bisphenol A-Type Unfilled, Room Temperature Cure, Semiflexible
SAE AMS3731/1B-1993 (Noncurrent)Potting Compound, Epoxy Bisphenol A-Type Unfilled, Room Temperature Cure
SAE AMS3731/5B-1993 (Noncurrent)Potting Compound, Epoxy Bisphenol A-Type Filled, Room Temperature Cure, Low Exotherm
SAE AMS3731/7B-1993 (Noncurrent)Potting Compound, Epoxy Bisphenol A-Type Filled, Room Temperature Cure, Low Shrinkage
SAE AMS3731/10B-1993 (Noncurrent)Potting Compound, Epoxy Bisphenol A-Type Unfilled, Room Temperature Cure, Semiflexible
SAE AMS3375B-2001 Adhesive/Sealant, Fluorosilicone Aromatic Fuel Resistant, One-Part Room Temperature Vulcanizing
SAE AMS1387A-2004 Remover, Anti-Galling Compound Aircraft Turbine Engine Components Room Temperature Application
SAE AMS1387-2011 REMOVER, ANTI-GALLING COMPOUND Aircraft Turbine Engine Components Room Temperature Application
SAE AMS3373/1A-2001 Compound, Silicone Rubber, Insulating and Sealing Oil and Reversion Resistant, Low Viscosity, Room Temperature Cure
SAE AMS3373/2A-2001 Compound, Silicone Rubber, Insulating and Sealing Oil and Reversion Resistant, Medium Viscosity, Room Temperature Cure
SAE AMS3373/1-1981 COMPOUND, SILICONE RUBBER, INSULATING AND SEALING Oil and Reversion Resistant, Low Viscosity, Room Temperature Cure
SAE AMS3373/2-1981 COMPOUND, SILICONE RUBBER, INSULATING AND SEALING Oil and Reversion Resistant, Medium Viscosity, Room Temperature Cure
SAE TS22-10-2008 TS22 Manufacturing Specification for Bolts 1100 MPa (159,000 lbf/in²) Ultimate Tensile Strength Minimum at Room Temperature
SAE TS22-11-2019 TS22 Manufacturing Specification for Bolts 1100 MPa (159,000 lbf/in²) Ultimate Tensile Strength Minimum at Room Temperature
SAE TS24-7-2019 TS24 Manufacturing Specification for Bolts 1275 MPa (185,000 lbf/in²) Tensile Strength at Room Temperature 1000 MPa (145,000 lbf/in²) Tensile Strength at 650°C
SAE TS128-6-2006 TS128 "All Metal" Self-Locking Nuts (UNJ Threads) 1100 MPa (160,000 lbf/in²) Minimum Tensile Strength at Room Temperature
SAE TS128-7-2019 TS128 "All-Metal" Self-Locking Nuts (UNJ Threads) 1100 MPa (160,000 lbf/in²) Minimum Tensile Strength at Room Temperature
SAE TS8-10-2004 TS8 Technical Specification for "All Metal" Self-Locking Nuts (UNJ Threads) 1100 MPa (160,000 lbf/in²) Minimum Tensile Strength at Room Temperature
SAE TS220-1-2005 TS220 Technical Specification for Self Locking Union Nuts (Unified Threads) Manufactured from INCO718 Material.1270 MPa (185000 lbf/in2) Minimum Tensile Strength at Room Temperature

SAE - SAE International, double antibody room temperature

SAE AMS3731/1C-2016 Potting Compound@ Epoxy Bisphenol A-Type Unfilled@ Room Temperature Cure
SAE AMS3731/7C-2016 Potting Compound@ Epoxy Bisphenol A-Type Filled@ Room Temperature Cure@ Low Shrinkage
SAE AMS3731/5C-2016 Potting Compound@ Epoxy Bisphenol A-Type Filled@ Room Temperature Cure@ Low Exotherm
SAE AMS3731/10C-2017 Potting Compound@ Epoxy Bisphenol A-Type Unfilled@ Room Temperature Cure@ Semiflexible

Military Standard of the People's Republic of China-General Armament Department, double antibody room temperature

GJB 9437-2018 Specification for room temperature curing two-component acrylic adhesives
GJB 1806-1993 Specification for high temperature anti-oxidation coating of niobium-hafnium alloy thrust chamber
GJB 1806A-2021 Specification for high temperature anti-oxidation coating of niobium-hafnium alloy thrust chamber

Indonesia Standards, double antibody room temperature

SNI 06-0243-1989 Test method of enamel resistance to weak acid at room temperature

Korean Agency for Technology and Standards (KATS), double antibody room temperature

KS K ISO 6925:2007 Textile floor coverings－Burning behaviour－Tablet test at ambient temperature
KS L ISO 16282:2012 Methods of test for dense shaped refractory products-Determination of resistance to abrasion at ambient temperature
KS L 1601-2006(2016) Fine ceramics(advanced ceramics, advanced technical ceramics)－Test method for compressive strength of monolithicceramics at room temperature
KS L 1601-2006(2021) Fine ceramics(advanced ceramics, advanced technical ceramics)－Test method for compressive strength of monolithicceramics at room temperature
KS C IEC 61788-24:2021 Superconductivity — Part 24: Critical current measurement — Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires

Danish Standards Foundation, double antibody room temperature

DS/EN 12833:2001 Skylight and conservatory roller shutters - Resistance to snow load - Test method
DS/ISO 6925:1985 Textile floor coverings. Burning behaviour. Tablet test at ambient temperature
DS/EN 843-1:1995 Advanced technical ceramics - Monolithic ceramics - Mechanical properties at room temperature - Part 1: Determination of flexural strength
DS/ENV 658-1:1993 Advanced technical ceramics. Mechanical properties of ceramic composites at room temperature. Part 1: Determination of tensile strength
DS/ENV 658-3:1993 Advanced technical ceramic. Mechanical properties of ceramic composites at room temperature. Part 3: Determination of flexural strength
DS/CEN/TS 843-9:2010 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Part 9: Method of test for edge-chip resistance
DS/EN 4688:2021 Aerospace series – Paints and varnishes – Corrosion resistant chromated two-components room temperature curing epoxy primer – High corrosion resistance for military application
DS/ENV 658-6:1993 Advanced technical ceramic. Mechanical properties of ceramic composites at room temperature. Part 6: Determination of shear strength by double-punch shearing
DS/EN 4689:2021 Aerospace series – Paints and varnishes – Two-components room temperature curing polyurethane finish – High flexibility and chemical agent resistance for military application

Lithuanian Standards Office , double antibody room temperature

LST EN 12833-2002 Skylight and conservatory roller shutters - Resistance to snow load - Test method
LST EN 4688-2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
LST EN 4689-2021 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
LST EN 4687-2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application

AENOR, double antibody room temperature

UNE-EN 12833:2001 Skylight and conservatory roller shutters - Resistance to snow load - Test method.

German Institute for Standardization, double antibody room temperature

DIN EN 12833:2001-10 Skylight and conservatory roller shutters - Resistance to snow load - Test method; German version EN 12833:2001
DIN EN ISO 16282:2008 Methods of test for dense shaped refractory products - Determination of resistance to abrasion at ambient temperature (ISO 16282:2007); German version EN ISO 16282:2008
DIN 51104:2010 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Determination of compressive strength
DIN EN 2002-001:2006 Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature; German and English version EN 2002-001:2005
DIN EN 843-1:2007 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Part 1: Determination of flexural strength; German version EN 843-1:2006
DIN 65463:2011 Aerospace - Studs with MJ thread, captive ring lock, titanium alloy, tensile strength 1 100 MPa, for temperatures up to 315 C
DIN EN 3019:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286) - Classification: 1100 MPa (at ambient temperature)/650 °C; German and English version EN 3019:2008
DIN EN 658-2:2003 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 2: Determination of compression properties; German version EN 658-2:2002
DIN 51105:2010 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Determination of flexural strength by the ring-on-ring test
DIN EN 658-1:1999 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 1: Determination of tensile properties; German version EN 658-1:1998
DIN EN 3020:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286), silver-plated - Classification: 1100 MPa (at ambient temperature)/650 °C; German and English version EN 3020:2008
DIN 65462:2011 Aerospace - Studs with MJ thread, captive ring lock, corrosion-resisting steel, tensile strength 1 100 MPa, for temperature up to 315 °C
DIN EN 4118:2006 Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature) / 650 °C; German and English version EN 4118:2004
DIN 65461:2011 Aerospace - Studs with MJ thread, captive ring lock, steel, nominal tensile strength 1 100 MPa, for temperature up to 235 °C
DIN EN 4084:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in alloy steel, cadmium plated, MoS<(Index)2> lubricated - Classification: 1100 MPa (at ambient temperature)/235 °C; German and English version EN 4084:2009
DIN EN 3724:2005 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS<(Index)2> coated - Strength class: 1100 MPa (at ambient temperature); German and English version EN 3724:2004
DIN EN 4688:2021-03 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application; German and English version EN 4688:2021
DIN 65537:1987-08 Aerospace; cheese head bolts with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65464:2011 Aerospace - Studs with MJ thread, ring locked, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 C; Text in German and English
DIN CEN/TS 843-9:2010-11*DIN SPEC 1158:2010-11 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Part 9: Method of test for edge-chip resistance; German version CEN/TS 843-9:2010
DIN EN 4687:2021-03 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application; German and English version EN 4687:2021
DIN 65438:1993-12 Aerospace; bihexagonal head bolts, close tolerance, with MJ-thread, short thread length, in titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN EN 4689:2021-03 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application; German and English version EN 4689:2021
DIN EN 3832:2005 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1550 MPa (at ambient temperature)/650 °C; German and English version EN 3832:2004
DIN 65439:1984-08 Aerospace; bihexagonal head bolts, close tolerance, with MJ-thread, medium thread length, in steel, nominal tensile strength 1250 MPa, for temperatures up to 235 °C
DIN 65440:1984-08 Aerospace; bihexagonal head bolts, close tolerance, with MJ-thread, medium thread length, in corrosion resisting steel, nominal tensile strength 1250 MPa, for temperatures up to 315 °C
DIN 65538:1987-08 Aerospace; cheese head bolts, close tolerance, with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C

Shandong Provincial Standard of the People's Republic of China, double antibody room temperature

DB37/T 3274.1-2020 Solar Greenhouse Construction Technical Specifications Part 1: Two-way

Association Francaise de Normalisation, double antibody room temperature

NF EN ISO 16496:2016 Verrerie de laboratoire - Récipients à double enveloppe à vide pour isolation thermique
NF EN ISO 8895:2006 Produits réfractaires isolants façonnés - Détermination de la résistance à l'écrasement à température ambiante
NF U57-064:1991 Greenhouses and greenhouse equipment. Stability requirements for the construction of single or multispan or double tunnel greenhouses covered with flexible or cold berdable plastic sheet.
NF EN 2909:1995 Série aérospatiale - Écrous bihexagonaux, à freinage interne, chambres, en acier résistant à chaud Fe-PA92HT (A286), argentés - Classification : 1 100 MPa (à température ambiante)/ 650 degrés Celsius.
NF L24-212*NF EN 2926:1996 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel fe-PA92HT (A286), silver plated. Classification : 900 MPa (at ambient temperature) / 650 degrees celsius.
NF L24-672*NF EN 2906:1994 Aerospace series. Nuts, bihexagonal, self-locking, in heat resisting steel fe-PA92HT (A286). Classification : 1100 MPa (at ambient temperature) / 650 degrees celsius.
NF L24-673*NF EN 2907:1996 Aerospace series. Nuts, bihexagonal, self-locking, in heat resisting steel fe-PA92HT (A286), silver plated. Classification : 1100 MPa (at ambient temperature) / 650 degrees celsius.
NF EN 3843:2011 Série aérospatiale - Écrous bihexagonaux, à freinage interne, avec chambrage, en acier résistant à chaud, passivés - Classification : 1 100 MPa (à température ambiante)/650 oC
NF L24-211*NF EN 2925:1994 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting steel fe-PA92HT (A286). Classification : 900 MPa (at ambient temperature) / 650 degrees celsius.
NF B41-206:1995 Advanced technical ceramics. Monolithic ceramics. Mechanical properties at room temperature. Part 1 : determination of flexural strength.
NF L24-231*NF EN 2929:1996 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy ni-P101HT (waspaloy). Classification : 1 210 MPa (at ambient temperature) / 730 degrees celsius.
NF L24-478*NF EN 3019:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286) - Classification : 1 100 MPa (at ambient temperature)/650 oC.
NF L24-669*NF EN 2908:1994 Aerospace series. Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel fe-PA92HT (A286). Classification : 1100 MPa (at ambient temperature) / 650 degrees celsius.
NF L24-221*NF EN 2927:1996 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy ni-P100HT (inconel 718). Classification : 1 275 MPa (at ambient temperature) / 650 degrees celsius.
NF L24-225*NF EN 3379:1996 Aerospace series. Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy ni-P101HT (waspaloy), for increased height nuts. Classification : 1210 MPa (at ambient temperature) / 730 degrees celsius.
NF L24-674*NF EN 3720:1995 Aerospace series. Nuts, bihexagonal, self-locking, in heat resisting steel fe-PA92HT (A286), MOS2 coated. Classification : 1 100 MPa (at ambient temperature) / 425 degrees celsius.
NF EN 2434-001:2012 Série aérospatiale - Peintures et vernis - Peinture de finition polyuréthane, à deux composants polymérisant à température ambiante - Partie 001 : exigences générales
NF EN 2434-004:2012 Série aérospatiale - Peintures et vernis - Peinture de finition polyuréthane, à deux composants, polymérisant à température ambiante - Partie 004 : haute flexibilité
NF L24-232*NF EN 2930:1996 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy ni-P101HT (waspaloy), silver plated. Classification : 1 210 MPa (at ambient temperature) / 730 degrees celsius.
NF L24-230*NF EN 3724:2005 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strenght class : 1 100 MPa (at ambient temperature).
NF L24-226*NF EN 3907:2005 Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MOS2 coated - Classification : 1 100 MPa (at ambient temperature) / 350 oC
NF L24-556*NF EN 3843:2011 Aerospace series - Nuts, bihexagonal, self-locking, with counterbore, in heat resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature)/650 oC
NF L24-670*NF EN 2909:1995 Aerospace series. Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel fe-PA92HT (A286), silver plated. Classification : 1 100 MPa (at ambient temperature) / 650 degrees celsius.
NF EN 2906:1994 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en acier résistant à chaud Fe-PA92HT (A286) - Classification : 1 100 MPa (à température ambiante)/650 degrés Celsius.
NF EN 3720:1995 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en acier résistant à chaud Fe-PA92HT (A286), revêtus MoS2 - Classification : 1 100 MPa (à température ambiante)/ 425 degrés Celsius.
NF EN 4119:2005 Série aérospatiale - Écrous bihexagonaux, à freinage interne, à chambrage profond, en acier résistant à chaud FE-PA2601 (A286), argentés sur filetage - Classification : 1 100 MPa (à température ambiante) / 650 oC
NF EN 3537:2010 Série aérospatiale - Écrous à river, à freinage interne, fixes, double patte, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification : 1 100 MPa (à température ambiante)/315 oC
NF EN 2907:1996 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en acier résistant à chaud Fe-PA92HT (A286), argentés - Classification : 1 100 MPa (à température ambiante) / 650 degrés Celsius.
NF L24-222*NF EN 2928:1996 Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy ni-P100HT (inconel 718), silver plated. Classification : 1 275 MPa (at ambient temperature) / 650 degrees celsius.
NF B43-203:2002 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 3 : determination of flexural strength.
NF B43-202:2003 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 2 : determination of compression properties.
NF L17-306:2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
NF EN 4084:2010 Série aérospatiale - Écrous à river, à freinage interne, fixes, double patte, avec chambrage, en acier, cadmiés, lubrifiés MoS2 - Classification : 1 100 MPa (à température ambiante)/235 oC
NF L24-479*NF EN 3020:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286), silver plated - Classification : 1 100 MPa (at ambient temperature)/650 oC
NF L24-671*NF EN 3721:1995 Aerospace series. Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel fe-PA92HT (A286), MOS2 coated. Classification : 1 100 MPa (at ambient temperature) / 425 degrees celsius.
NF EN 2908:1994 Série aérospatiale - Écrous bihexagonaux, à freinage interne, chambres, en acier résistant à chaud Fe-PA92HT (à 286) - Classification : 1 100 MPa (à température ambiante)/650 degrés Celsius.
NF EN 4120:2005 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH1302 (Waspaloy), argentés sur filetage - Classification : 1 210 MPa (à température ambiante) / 730 oC
NF EN 2436-001:2006 Série aérospatiale - Peintures et vernis - Peinture primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 001 : exigences générales
NF EN 2434-003:2012 Série aérospatiale - Peintures et vernis - Peinture de finition polyuréthane, à deux composants polymérisant à température ambiante - Partie 003 : flexible à résistance au fluide pour intérieur
NF EN 3907:2005 Série aérospatiale - Vis à tête bihexagonale, fût normal, filetage long, en alliage de titane TI-P64001, revêtues MoS2 - Classification : 1 100 MPa (à température ambiante) / 350 oC
XP B41-206-9*XP CEN/TS 843-9:2010 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Part 9 : method of test for edge-chip resistance
NF B43-203*NF EN ISO 17138:2022 Fine ceramics (advanced ceramics, advanced technical ceramics) - Mechanical properties of ceramic composites at room temperature - Determination of flexural strength
NF L17-307:2021 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
NF B43-206:1993 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 6:Determination of shear strength by double-punch shearing
NF L22-525:2001 Aircraft bolts and nuts - Nuts, bihexagonal, self-locking, ISO M threads, fine pitch threads, in steel, cadmium plated, MoS2 lubricated - Classification : 1 100 MPa (at ambiant temperature) / 235 oC
NF L24-224*NF EN 3063:1994 Aerospace series. Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy ni-P101HT (waspaloy). Classification : 1210 MPa (at ambient temperature) / 730 degrees celsius.
NF EN 4117:2005 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718), argentés sur filetage - Classification : 1 550 MPa (à température ambiante) / 600o C
NF EN 3721:1995 Série aérospatiale - Écrous bihexagonaux, à freinage interne, chambres, en acier résistant à chaud Fe-PA92HT (A286), revêtus MoS2 - Classification : 1 100 MPa (à température ambiante)/ 425 degrés Celsius.
NF EN 3013:1996 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel Ni-P101HT (Waspaloy), argentés - Classification : 1 210 MPa (à température ambiante) / 730 degrés Celsius.
NF EN 4136:2010 Série aérospatiale - Vis à tête bihexagonale normale, tige normale à tolérance large, filetage long, en acier allié, cadmiées - Classification : 1 100 MPa (à température ambiante)/235oC
NF EN 2434-002:2012 Série aérospatiale - Peintures et vernis - Peinture de finition polyuréthane, à deux composants polymérisant à température ambiante - Partie 002 : tenue chimique aux fluides
NF EN 2925:1994 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en acier résistant à chaud Fe-PA92HT (A286) - Classification : 900 MPa (à température ambiante)/ 650 degrés Celsius.
NF EN 3724:2005 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage de titane TI-P64001, revêtues MoS2 - Classe de résistance : 1 100 MPa (à température ambiante)
XP CEN/TS 843-9:2010 Céramiques techniques avancées - Propriétés mécaniques des céramiques monolithiques à température ambiante - Partie 9 : méthode d'essai de la résistance à l'écaillage des bords
NF L24-147*NF EN 4136:2010 Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification : 1 100 MPa (at ambient temperature)/235 oC.
NF L22-519:2000 Aircraft bolts and nuts - Bihexagonal nuts, self-locking, ISO M or ISO MJ threads, in steel, cadmium plated, MoS2 lubricated - Classification : 1 550 MPa (at ambient temperature) / 235 oC
NF C31-888-24*NF EN IEC 61788-24:2018 Superconductivity - Part 24 : critical current measurement - Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires
NF EN 2929:1996 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage résistant à chaud à base de nickel Ni-P101HT (Waspaloy) - Classification : 1210 MPa (à température ambiante) / 735 degrés Celsius.
NF EN 2926:1996 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en acier résistant à chaud Fe-PA92HT (A286) argentées - Classification : 900 MPa ( à température ambiante ) / 650 degré Celsius.
NF L24-473*NF EN 2680:2006 Aerospace series - Nuts, anchor, self-locking, floating, self-aligning two lug, in alloy steel, cadmium plated, MoS2 lubricated - Classification : 900 MPa (at ambient temperature) / 235 oC.
NF L24-488*NF EN 3834:2010 Aerospace series - Nuts, anchor, self-locking, floating, two lug, incremental counterbore, in corrosion resisting steel, MoS2 lubricated - Classification : 900 MPa (at ambient temperature)/315 oC
NF L24-466*NF EN 2865:2010 Aerospace series - Nuts, anchor, self-locking, floating, two lugs, with counterbore, in heat resisting steel, MoS2 lubricated - Classification : 1 100 MPa (at ambient temperature)/315 oC
NF L17-305:2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application
NF EN 4012:2005 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718), revêtus MoS2 - Classification : 1 550 MPa (à température ambiante) / 425 o C
NF EN 3538:2010 Série aérospatiale - Écrous à river, à freinage interne, fixes, double patte, série reduite, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification : 1 100 MPa (à température ambiante)/315 oC
NF EN 2879:2017 Série aérospatiale - Écrous à river, à freinage interne, étanches à l'air, flottants, double patte, avec chambrage, en acier résistant à la corrosion, passivés, lubrifiés MoS2 - Classification: 900 MPa (à température ambiante) / 235 oC
NF EN 3012:1996 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel Ni-P101HT (Waspaloy) - Classification : 1 210 MPa (à température ambiante) / 730 degrés Celsius.
NF EN 3435:2010 Série aérospatiale - Écrous à river, à freinage interne, flottants, double patte, série réduite, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification : 1 100 MPa (à température ambiante)/315 oC
NF EN 3832:2005 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718) - Classification : 1 550 MPa (à température ambiante) / 650 oC
NF L24-223*NF EN 3832:2005 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification : 1 550 MPa (at ambient temperature) / 650 oC.
NF L24-468*NF EN 3537:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, MoS2 lubricated - Classification : 1 100 MPa (at ambient temperature)/315 oC
NF EN 4009:2005 Série aérospatiale - Vis à tête bihexagonale, fût à tolérance serrée, filetage moyen, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718) - Classification : 1 550 MPa (à température ambiante) / 650 oC
NF EN 3444:2007 Série aérospatiale - Vis à tête bihexagonale large, tige normale à tolérance serrée, filetage moyen, en alliage résistant à chaud à base de nickel, passivées - Classification : 1250 MPa (à température ambiante)/650oC
NF EN 4137:2010 Série aérospatiale - Vis à tête bihexagonale normale, à tige dégagée, filetage long, en alliage de titane, anodisées, lubrifiées MoS2 - Classification : 1 100 MPa (à température ambiante)/315 oC
NF EN 2930:1996 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage résistant à chaud à base de nickel Ni-P101HT (Waspaloy), argentées - Classification : 1210 MPa (à température ambiante) / 735 degrés Celsius.
NF EN 4688:2021 Série aérospatiale - Peintures et vernis - Peinture primaire époxy anticorrosion chromatée à deux composants polymérisant à température ambiante - Haute résistance à la corrosion pour applications militaires
NF L24-474*NF EN 2881:2006 Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated - Classification : 900 MPa (at ambient temperature) / 120 oC.
NF EN 2264:1997 Série aérospatiale - Écrous à river, à freinage interne, flottants, double patte, à chambrage trés profond, en acier allié, cadmiés, lubrifiés MoS2 - Classification : 900 MPa (à température ambiante) / 235 degrés Celsius.
NF EN 3239:1996 Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel Ni-P101HT (Waspaloy), à filetage argenté - Classification : 1 210 MPa (à température ambiante) / 730 degrés Celsius.
NF EN 2927:1996 Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage résistant à chaud à base de nickel Ni-P100HT (Inconel 718) - Classification : 1275 MPa (à température ambiante) 650 degrés Celsius.
NF L22-587:2000 Aircraft bolts and nuts - Nuts, anchor, self-locking, two lug, with counterbore, ISO M or ISO MJ threads, in corrosion resisting steel, silver plated - Classification : 1 100 MPa (at ambient temperature) / 425 oC.
NF L22-567:2001 Aircraft bolts and nuts - Nuts, anchor, self-locking, two lug, with counterbore, ISO M or ISO MJ threads, in steel, cadmium plated, MoS2 lubricated - Classification : 1 100 MPa (at ambiant temperature) / 235 oC.
NF L24-146*NF EN 4135:2010 Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification : 1 100 MPa (at ambient temperature)/315oC
NF L24-470*NF EN 4084:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated - Classification : 1 100 MPA (at ambient temperature)/235 oC
NF EN 4687:2021 Série aérospatiale - Peintures et vernis - Peinture primaire sans chromate (non anticorrosion) à deux composants polymérisant à température ambiante - Peinture primaire sans chromate pour applications militaire
NF EN 3063:1994 Série aérospatiale - Vis à tête bihexagonale, tige à tolérance serrée, filetage moyen, en alliage résistant à chaud à base nickel Ni-P101HT (Waspaloy) - Classification : 1210 MPa (à température ambiante)/730 degrés Celsius.
NF EN 4689:2021 Série aérospatiale - Peintures et vernis - Peinture de finition polyuréthane à deux composants polymérisant à température ambiante - Haute flexibilité et résistance aux substances chimiques pour applications militaires
NF EN 4135:2010 Série aérospatiale - Vis à tête bihexagonale normale, tige normale à tolérance large, filetage moyen, en alliage de titane, anodisées, lubrifiées MoS2 - Classification : 1 100 MPa (à température ambiante)/315oC
NF EN ISO 18608:2022 Céramiques techniques - Propriétés mécaniques des céramiques composites à température ambiante sous pression atmosphérique - Evaluation de la résistance à la propagation de fissure par un essai de sensibilité à l'entaille

Japanese Industrial Standards Committee (JISC), double antibody room temperature

JIS R 1621:1995 Testing methods for bending fatigue of fine ceramics at room temperature
JIS H 7601-1:2002 Method of tensile test for intermetallic compounds -- Part 1: Room temperature tensile test
JIS H 7303:2002 Superconductivity -- Part 6: Mechanical properties measurement -- Room temperature tensile test of Cu/Nb-Ti composite superconductors
JIS H 7303:2013 Superconductivity -- Part 6: Mechanical properties measurement -- Room temperature tensile test of Cu/Nb-Ti composite superconductors

Guizhou Provincial Standard of the People's Republic of China, double antibody room temperature

DB52/T 953-2014 Technical regulations for inoculation identification of hot pepper varieties against blight in greenhouse
DB52/T 955-2014 Technical Regulations for Inoculation Identification of Capsicum Varieties Resistant to Bacterial Wilt

European Committee for Standardization (CEN), double antibody room temperature

DD ENV 658-6-1993 Advanced Technical Ceramics - Mechanical Properties of Ceramic Composites at Room Temperature - Part 6 : Determination of Shear Strength by Double-Punch Shearing
EN 2925:1994 Bolts, Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Classification : 900MPa (at Ambient Temperature) /650 Degrees C
prEN 843-1-1992 Advanced technical ceramics; mechanical properties of monolithic ceramics at room temperature; part 1: determination of flexural strength
EN 3019:2008 Aerospace series - Self-locking plate nuts, floating, two-lug, in heat resisting steel FE-PA92HT (A286) - Classification: 1 100 MPa (at ambient temperature)/650 癈
DD ENV 658-3-1992 Advanced technical ceramics; mechanical properties of ceramic composites at room temperature; part 3: determination of flexural strength
DD ENV 658-2-1993 Advanced Technical Ceramics - Mechanical Properties of Ceramic Composites at Room Temperature - Part 2: Determination of Compressive Strength
EN 3843:2010 Aerospace series - Nuts, bihexagonal, self-locking, with counterbore, in heat resisting steel, passivated - Classification: 1100 MPa (at ambient temperature) / 650 °C
CEN/TS 843-9:2010 Advanced technical ceramics - Mechanical properties of monolithic ceramics at room temperature - Part 9: Method of test for edge-chip resistance
EN 3832:2004 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C
EN 3538:2010 Aerospace series - Nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
EN 3832:2003 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C
EN 2879:2017 Aerospace series - Nuts@ anchor@ self-locking@ air resistant@ sealing@ floating@ two lug@ with counterbore@ in corrosion resisting steel@ passivated@ MoS2 lubricated - Classification: 900 MPa (at ambient temperature) / 235 ��
DD ENV 658-4-1992 Advanced Technical Ceramics - Mechanical Properties of Ceramic Composites at Room Temperature - Part 4: Determination of Shear Strength by Compression Loading of Notched Specimens
EN 4012:2004 Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P100HT (Inconel 718), MoS2 coated - Classification: 1550 MPa (at ambient temperature)/425 °C
EN 2870:1996 Aerospace Series - Bolts, Normal Bihexagonal Head, Close Tolerance Normal Shank, Short Thread, in Titanium Alloy, Anodized, MoS2 Lubricated - Classification: 1100 MPa (at Ambient Temperature) /315 Degrees C
EN 3379:1996 Aerospace series - Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), for increased height nuts - Classification: 1210 MPa (at ambient temperature)/730 °C
EN 4012:2003 Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P100HT (Inconel 718), MoS2 coated - Classification: 1 500 MPa (at ambient temperature)/425 degrees C
DD ENV 658-5-1993 Advanced technical ceramics; mechanical properties of ceramic composites at room temperature; part 5: determination of shear strength by short span bend test (three-point)

Military Standards (MIL-STD), double antibody room temperature

DOD A-A-53474-1988 BEAD, GLASS, LABORATORY, (PLASTIC SPECTACLE FRAME WARMER)

Xinjiang Provincial Standard of the People's Republic of China, double antibody room temperature

DB65/T 2970-2009 Green Food Technical Specification for Agaricus bisporus.Lange.Sing Production in Greenhouse in Northern of Xinjiang

BR-ABNT, double antibody room temperature

ABNT MB-1308-1980

(U.S.) Ford Automotive Standards, double antibody room temperature

FORD ESB-M2G189-A-2014 ADHESIVE, URETHANE - TWO COMPONENT - ROOM TEMPERATURE CURING - STRUCTURAL ***TO BE USED WITH FORD WSS-M99P1111-A***

RU-GOST R, double antibody room temperature

GOST R 57802-2017 Ceramic composites. Test method for determination of transthickness tensile strength at ambient temperature
GOST R 53065.1-2008 Refractory products with less than 45 % true porosity. Method for determination of compressive strength at room temperature. Part 1. Test without packings
GOST R 53065.2-2008 Refractory products with less than 45 % true porosity. Method for determination of compressive strength at room temperature. Part 2. Test with packings

PL-PKN, double antibody room temperature

PN M77300-07-1992 Household enamel utensils made from ironplate , Kinds and methods of enamel coating Determination of resistance to citric acid at room temperature
PN-EN 4688-2021-06 E Aerospace series -- Paints and varnishes -- Corrosion resistant chromated two-components room temperature curing epoxy primer -- High corrosion resistance for military application
PN-EN 4689-2021-06 E Aerospace series -- Paints and varnishes -- Two-components room temperature curing polyurethane finish -- High flexibility and chemical agent resistance for military application

AT-ON, double antibody room temperature

ONORM ENV 658-2-1993 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 2: Determination of compressive strength
OENORM EN 4688-2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
ONORM ENV 658-6-1993 Advanced technical ceramics - Mechanical properties of ceramic composites at room temperature - Part 6: Determination of shear strength by double-punch shearing
OENORM EN 4687-2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application
ONORM EN 3052-1994 Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated. Classification: 1100 MPa (at ambient temperature) / 425 degree C

Aerospace, Security and Defence Industries Association of Europe (ASD), double antibody room temperature

ASD-STAN PREN 3019-1992 Aerospace Series Self-Locking Plate Nuts, Floating, Two-Lug, in Heat Resisting Steel FE-PA92HT (A286) Classification : 1 100 MPa (at Ambient Temperature) /650 Degrees C (Issue P 2)
ASD-STAN PREN 3020-1992 Aerospace Series Self-Locking Plate Nuts, Floating, Two-Lug, in Heat Resisting Steel FE-PA92HT (A286), Silver Plated Classification : 1 100 MPa (at Ambient Temperature) /650 Degrees C (Issue P 2)
ASD-STAN PREN 4390-1997 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Self-Aligning, Two Lug, in Heat Resisting Steel, Silver Plated, Classification : 900 MPa (at Ambient Temperature) / 425 Degrees Celsius (Edition P 1)

CH-SNV, double antibody room temperature

SN EN 4688-2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
SN EN 4689-2021 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
SN EN 4687-2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application

IT-UNI, double antibody room temperature

UNI EN 4688-2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
UNI EN 4689-2021 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
UNI EN 4687-2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application

International Electrotechnical Commission (IEC), double antibody room temperature

IEC 61788-24:2018 Superconductivity - Part 24: Critical current measurement - Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires

ES-UNE, double antibody room temperature

UNE-EN 4688:2021 Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application (Endorsed by Asociación Española de Normalización in February of 2021.)
UNE-EN 4687:2021 Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components room temperature curing primer - Chromate free primer for military application
UNE-EN IEC 61788-24:2018 Superconductivity - Part 24: Critical current measurement - Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires (Endorsed by Asociación Española de Normalización in October of 2018.)
UNE-EN 4689:2021 Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application (Endorsed by Asociación Española de Normalización in February of 2021.)

NL-NEN, double antibody room temperature

NVN-ENV 658-6-1994 Advanced technical ceramics. Mechanical properties of ceramic composites at room temperature. Part 6: Determination of shear strength by double-punch shearing

European Committee for Electrotechnical Standardization（CENELEC）, double antibody room temperature

EN IEC 61788-24:2018 Superconductivity - Part 24: Critical current measurement - Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires

KR-KS, double antibody room temperature

KS C IEC 61788-24-2021 Superconductivity — Part 24: Critical current measurement — Retained critical current after double bending at room temperature of Ag-sheathed Bi-2223 superconducting wires