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mp and mpa

mp and mpa, Total:498 items.

In the international standard classification, mp and mpa involves: Fasteners for aerospace construction, Materials for aerospace construction, Plastics, Fluid power systems, Fuels, Road vehicle systems, Fasteners, Equipment for the chemical industry, Valves.

U.S. Military Regulations and Norms, mp and mpa

ARMY MIL-C-63286 (3)-1982 CARTRIDGE, 105MM, HEAT-T-MP, M456A2 LOADING, ASSEMBLING AND PACKING
ARMY MIL-P-63448 A NOTICE 2-1997 PROJECTILE, 105MM, HEAT-T-MP, M456A2 SPIKE AND CAP ASSEMBLY
ARMY MIL-P-63448 A VALID NOTICE 1-1989 PROJECTILE, 105MM, HEAT-T-MP, M456A2 SPIKE AND CAP ASSEMBLY
ARMY MIL-P-63448 A-1984 PROJECTILE, 105MM, HEAT-T-MP, M456A2 SPIKE AND CAP ASSEMBLY
ARMY MIL-P-46458 F NOTICE 1-1997 PROPELLANT M30 FOR USE IN CARTRIDGE, 105MM, HEAT-T, M456A1 HEAT-T-MP, M456A1E2 AND TP-T, M490
ARMY MIL-P-46458 F (3)-1990 PROPELLANT M30 FOR USE IN CARTRIDGE, 105MM, HEAT-T, M456A1 HEAT-T-MP, M456A1E2 AND TP-T, M490
ARMY MIL-P-46458 F-1980 PROPELLANT M30 FOR USE IN CARTRIDGE, 105MM, HEAT-T, M456A1 HEAT-T-MP, M456A1E2 AND TP-T, M490

Professional Standard - Electron, mp and mpa

SJ/T 31378-1994 Requirements of readiness and methods of inspection and assessment for SM110-MP shock machine tables

British Standards Institution (BSI), mp and mpa

BS A 314:1997 Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 °C, 450 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/425 °C, 900 MPa (at ambient tempe
BS ISO 9609:2016 Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature) /120 degrees C, 450 MPa (at ambient temperature) /235 degrees C, 600 MPa (at ambient temperature) /425 degrees C, 9
BS EN ISO 14529-2:2000 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Preparation of test specimens and determination of properties
BS ISO 9618:2016 Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 degrees C, 450 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperature)/425
BS ISO 6150:2018 Pneumatic fluid power. Cylindrical quick-action couplings for maximum working pressures of 1 MPa, 1,6 MPa, and 2,5 MPa (10 bar, 16 bar and 25 bar). Plug connecting dimensions, specifications, application guidelines and testing
BS EN 2209:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa Rm 1100 MPa - Sheets, strips and plates - 0,5 mm a 20 mm
BS EN 2209:2008 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa Rm 1100 MPa - Sheets, strips and plates - 0,5 mm a 20 mm
BS ISO 8132:2006 Hydraulic fluid power - Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series - Mounting dimensions for accessories
BS 3S 145:1996+A2:2015 Specification for Chromium-nickel-copper-molybdenum corrosion resisting steel (precipitation hardening) billets, bars, forgings and parts (1270 MPa to 1470 MPa)
BS ISO 8132:2014 Hydraulic fluid power. Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
21/30423405 DC BS ISO 8132. Hydraulic fluid power. Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
BS A 321:1997 Nuts, anchor, self-locking, floating, self-aligning, single lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235°C, 900 MPa (at ambient temperature)/315°C and 900 MPa (at ambient temperature)/425°C. Dimensions
BS A 334:1999 Nuts, anchor, self-locking, fixed, 90° corner, 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 EN 4627:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De 200 mm. 1 150 MPa Rm 1 300 MPa
BS EN 4631:2013 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De 200 mm. 900 MPa Rm 1050 MPa
BS EN 4630:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De 200 mm. 900 MPa Rm 1 050 MPa
BS ISO 8132:2022 Tracked Changes. Hydraulic fluid power. Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
BS EN 4720:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De 200 mm. 1 150 MPa Rm 1 300 MPa
BS EN 4721:2014 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted and electroslag remelted (ESR). Hardened and tempered. Bar. De 200 mm. 900 MPa Rm 1 050 MPa
BS A 345:1999 Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235°C, 1100 MPa (at ambient temperature)/315°C, 1100 MPa (at ambient temperature)/425°C. Dimensions
BS EN 4628:2013 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De 200 mm. 1150 MPa Rm 1300 MPa
BS 7504:1995 Hydraulic fluid power - Four-screw, one-piece square flange connections for use at pressures of 25 MPa and 40 MPa (250 bar and 400 bar)
BS A 340:1999 Nuts, anchor, self-locking, fixed, 90° corner, reduced series, 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 A 337:1999 Nuts, anchor, self-locking, floating, single 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 A 330:1999 Nuts, anchor, self-locking, floating, two lug, with incremental counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/235°C, 900 MPa (at ambient temperature)/315°C and 900 MPa (at ambient temperature)/425°C. Dimensions
BS ISO 12273:2010 Aerospace. 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 and 900 MPa (at ambient temperature)/425 °C. Dimensions
BS A 329:1999 Nuts, anchor, self-locking, fixed, single 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
18/30383424 DC BS EN 3524. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Sheet and strip. 2 mm ≤ a ≤ 6 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
BS A 339:1999 Nuts, anchor, self-locking, floating, two lug, reduced series, 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 A 336:1999 Nuts, anchor, self-locking, fixed, 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 A 338:1999 Nuts, anchor, self-locking, fixed, two lug, reduced series, 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 2S 510:1970 Specification for carbon steel sheet and strip (430/540 MPa) (suitable for welding)
19/30408756 DC BS EN 4890. Aerospace series. Steel X4CrNiMo16-5-1. Air melted. Hardened and tempered. Sheets and plates. 0,6 mm ≤ a ≤ 50 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
21/30431249 DC BS EN 3524. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Sheets and strips. 2 mm ≤ a ≤ 6 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
21/30442582 DC BS EN 3361. Aerospace series. Steel X5CrNiCu15 5 (1.4545). Consumable electrode remelted. Solution treated and precipitation treated. Sheets and strips. a ≤ 6mm. 1 070 MPa ≤ Rm ≤ 1 220 MPa
21/30435499 DC BS EN 4628. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
19/30395270 DC BS EN 4627. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
21/30435496 DC BS EN 4627. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 Mpa
19/30395271 DC BS EN 4628. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
19/30395273 DC BS EN 4630. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
19/30395274 DC BS EN 4631. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
BS 3TA 2:2009 Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa)
21/30436446 DC BS EN 4630. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
21/30436449 DC BS EN 4631. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bars. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
BS EN 3666:2020 Aerospace series. Heat resisting alloy NI-PH2601. Solution treated and cold worked. Bar for forged fasteners. D ≤ 50 mm. 1 550 MPa ≤ Rm ≤ 1 830 MPa
BS EN 2952:2019 Aerospace series. Heat resisting alloy NI-PH2601. Solution treated and cold worked. Bar for forged fasteners. D ≤ 50 mm. 1 270 MPa ≤ Rm ≤ 1 550 MPa
BS EN 4627:2022 Tracked Changes. Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 1 150 MPa ≤ Rm ≤ 1 300 MPa
18/30383425 DC BS EN 3525. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Plate. 6 mm < a ≤ 20 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
BS EN 3528:2013 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D 150 mm. 1750 MPa Rm 2000 MPa
BS 2TA 52:2009 Specification for sheet and strip of titanium- copper alloy (tensile strength 690-920 MPa)
BS 3TA 6:2009 Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa)
BS A 327:1998 Nuts, bihexagonal, self-locking, with counterbore and MJ threads, classifications: 1100 MPa (at ambient temperature)/425°C, 1100 MPa (at ambient temperature)/650°C, 1210 MPa (at ambient temperature)/425°C, 1210 MPa (at ambient temperature)/730°C, 1...
BS 3TA 1:2009 Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)
BS ISO 12277:2000 Aerospace - Gang channel, self-locking, floating, standard series, with counterbore, classifications - 1100 MPa (at ambient temperature)/120 °C, 1100 MPa (at ambient temperature)/235 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions
18/30383423 DC BS EN 3523. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Bar for machining. De ≤ 100 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
21/30431252 DC BS EN 3525. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Plates. 6 mm ≤ a ≤ 20 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
20/30420958 DC BS EN 4890. Aerospace series. Steel X4CrNiMo16-5-1. Air melted. Hardened and tempered. Sheets. 0,3 mm ≤ a ≤ 6 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
21/30431246 DC BS EN 3523. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Bar for machining. De ≤ 100 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
BS EN 4244:2020 Aerospace series. Heat resisting alloy FE-PM1708. Vacuum arc remelted. Hardened and tempered. Bars. a or D ≤ 200 mm. 1 000 MPa ≤ Rm ≤ 1 140 MPa
BS EN 3120:2012 Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm D 51 mm. 690 MPa Rm 1030 MPa
BS EN 3529:2010 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Forgings - a or D 150 mm - 1750 MPa Rm 2000 MPa
BS S 534:1969 Specification for chromium-molybdenum steel sheet and strip 880/1080 MPa suitable for welding
21/30442588 DC BS EN 3479. Aerospace series. Steel X5CrNiCu15 5 (1.4545). Consumable electrode remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 20 mm. 1 070 MPa ≤ Rm ≤ 1 220 MPa
BS EN 3470:2019 Aerospace series. Steel FE-PM1503 (X3CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings - a or D ≤ 150 mm. 1 200 MPa ≤ Rm ≤ 1 400 MPa
BS EN 3532:2007 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5).Vacuum induction melt ed and vacuum arc remelted - Solution treated and precipitation treated.P late - 6 mm $2J a 40 mm - 1750 MPa Rm 2000 MPa
BS 2S 511:1970 Specification for deep drawing carbon steel sheet and strip (280/400 MPa) (suitable for welding)
BS S 536:1970+A2:2013 Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel sheet and strip (500 MPa)
BS S 537:1970+A2:2013 Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel sheet and strip (500 MPa)
19/30395307 DC BS EN 4884. Aerospace series. Steel X3CrNiMoAl 13-8-2. Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D ≤ 200 mm. 1 200 MPa ≤ Rm ≤ 1 350 MPa

Society of Automotive Engineers (SAE), mp and mpa

SAE AMS6386C-2000 Steel Sheet and Plate Low Alloy, Heat Treated 90,000 psi (621 MPa) and 100,000 psi (690 MPa) Yield Strength
SAE MA3376B-2012 Bolts & Screws, UNS G87400 Tensile Strength 860 MPa & 1000 MPa Procurement Specification, Metric
SAE MA1943A-1990 Nuts, Self-Locking, UNS N07001 730 Degrees C, 1100 MPa, and 1210 MPa Procurement Specification for, Metric FSC 5310
SAE MA1943A-2012 Nuts, Self-Locking, UNS N07001 730°C, 1100 MPa, and 1210 MPa Procurement Specification For, Metric
SAE MA3376B-1997 Bolts& Screws, UNS G87400 Tensile Strength 860 MPa& 1000 MPa Procurement Specification, Metric UNS G87400; FSC 5306
SAE AMS6386B-1994 STEEL SHEET AND PLATE Low Alloy, Heat Treated 90,000 psi (621 MPa) and 100,000 psi (690 MPa) Yield Strength
SAE AMS6386C-2011 Steel Sheet and Plate Low Alloy, Heat Treated 90,000 psi (621 MPa) and 100,000 psi (690 MPa) Yield Strength
SAE MA1943-1987 NUT, SELF LOCKING - UNS N07001, 760°C, 1250 MPa & 1100 MPa, MJ THREAD, PROCUREMENT SPECIFICATION FOR, METRIC
SAE AMS4983E-2011 Titanium Alloy, Forgings 10V-2Fe-3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged, 180 ksi (1241 MPa) Tensile Strength
SAE J518/1-2013 Hydraulic Flanged Tube, Pipe, and Hose Connections, 4-Screw Flange Connection Part 1: 3.5 MPa to 35 MPa (Code 61)
SAE J518-1-2013 Hydraulic Flanged Tube, Pipe, and Hose Connections, 4-Screw Flange Connection Part 1: 3.5 MPa to 35 MPa (Code 61)
SAE MA3378B-1995 BOLTS AND SCREWS, UNS N07001 730°C, 1210 MPa Procurement Specification For, Metric
SAE AMS4901T-2015 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa)
SAE AMS4901M-1995 TITANIUM SHEET, STRIP, AND PLATE Commercially Pure Annealed, 70.0 ksi (485 MPa)
SAE AMS4921G-1995 TITANIUM BARS, WIRE, FORGINGS, AND RINGS Commercially Pure 70.0 ksi (483 MPa) Yield Strength
SAE AMS4921P-2020 Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength
SAE AMS4908F-1988 Titanium Alloy Sheet and Strip, 8Mn, Annealed, 110 ksi (760 MPa) Yield Strength
SAE AMS4901P-2006 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70 ksi (485 MPa)
SAE AMS4908E-1993 TITANIUM ALLOY SHEET AND STRIP 8Mn Annealed, 110,000 psi (760 MPa) Yield Strength
SAE MA3374-1995 BOLTS & SCREWS, UNS S66286 650°C, 900 MPa, MJ Thread, Procurement Specification for, Metric
SAE AMS5906-2000 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 185 ksi (1276 MPa) Tensile
SAE AMS4921R-2021 Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700)
SAE AMS4901S-2011 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70 ksi (485 MPa)
SAE AMS5518N-2020 Steel, Corrosion Resistant, Sheet and Strip 18Cr - 8Ni Cold Rolled, 150 ksi (1034 MPa) Tensile Strength
SAE MA1568-2012 Nut, Self Locking - UNS S66286, 425°C & 650°C, 1100 MPa, MJ Thread, Procurement Specification For, Metric
SAE AMS6317G-2003 Steel Bars and Forgings 1.8Ni 0.25Mo (0.38-0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6317F-1995 STEEL BARS AND FORGINGS 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6317L-2022 Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS4940D-2023 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 25.0 ksi (172 MPa) Yield Strength
SAE AMS4902M-2023 Titanium Sheet, Strip, and Plate Commercially Pure Annealed 40.0 ksi (276 MPa) Yield Strength
SAE AMS4926P-2019 Titanium Alloy, Bars, Wire, and Rings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength
SAE AMS6472D-2001 Steel Bars and Forgings, Nitriding 1.6Cr 0.35Mo 1.1Al (0.38-0.43C) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
SAE AMS6472C-1995 STEEL BARS AND FORGINGS, NITRIDING 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
SAE AMS4921M-2012 Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700)
SAE AMS6317J-2012 Steel Bars and Forgings 1.8Ni 0.25Mo (0.38-0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE MA1568-1987 Nut, Self Locking - UNS S66286, 425 Degrees C& 650 Degrees C, 1100 MPa, MJ Thread, Procurement Specification for, Metric FSC 5310
SAE MA3377A-1995 Bolts and Screws, Nickel Alloy UNS NO7718, Tensile Strength 1275 MPa Procurement Specification, Metric
SAE MA3377A-2006 Bolts and Screws, Nickel Alloy UNS N07718, Tensile Strength 1275 MPa Procurement Specification, Metric
SAE MA3377B-2012 Bolts and Screws, Nickel Alloy UNS N07718, Tensile Strength 1275 MPa Procurement Specification, Metric
SAE AMS4900K-1995 TITANIUM SHEET, STRIP, AND PLATE Commercially Pure Annealed, 55.0 ksi (379 MPa) Yield Strength
SAE AMS4902F-1995 TITANIUM SHEET, STRIP, AND PLATE Commercially-Pure Annealed 40.0 ksi (276 MPa) Yield Strength
SAE AMS5905-2000 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 175 ksi (1207 MPa) Tensile Strength
SAE AMS5519G-1979 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 8Ni (SAE 30301) Cold Rolled, 185,000 psi (1276 MPa) Tensile Strength
SAE AMS5518F-1984 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 8Ni (SAE 30301) Cold Rolled, 150,000 psi (1035 MPa) Tensile Strength
SAE AMS5902-2000 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 8Ni (SAE 30301) Cold Rolled, 175 ksi (1207 MPa) Tensile Strength
SAE AMS5517G-1984 STEEL SHEET AND STRIP, CORROSION RESISTANT 18Cr - 8Ni (SAE 30301) Cold Rolled, 125,000 psi (860 MPa) Tensile Strength
SAE AMS6346A-2009 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
SAE AMS4900S-2023 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 55 ksi (379 MPa) Yield Strength
SAE AMS6346C-2018 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength

German Institute for Standardization, mp and mpa

DIN 65393:2002 Aerospace - Thread inserts with MJ thread, ring locked, screw-locking, steel; Classification: 900 MPa/1100 MPa/1250 MPa/1550 MPa/235 °C
DIN EN ISO 14529-1:2000 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 1: Designation system and basis for specifications (ISO 14529-1:1999); German version EN ISO 14529-1:1999
DIN EN ISO 14529-1:2000-08 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 1: Designation system and basis for specifications (ISO 14529-1:1999); German version EN ISO 14529-1:1999
DIN 65160:2018-02 Aerospace series - Screws in material 1.4534 - Nominal tensile strength 1 220 MPa, 1 400 MPa and 1 550 MPa for temperatures up to 315 °C - Technical specifications
DIN 65394:2003 Aerospace - Thread inserts, with MJ thread, ring locked, screw-locking, corrosion-resisting steel; Classification: 900 MPa/1100 MPa/1250 MPa/1550 MPa/315 °C/425 °C
DIN EN ISO 14529-2:2000 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 2: Preparation of test specimens and determination of properties (ISO 14529-2:1999); German version EN ISO 14529-2:1999
DIN 65251:2013 Aerospace series - Bolts, with MJ threads, in titanium alloys, strength class 900 MPa and 1 100 MPa - Technical specification
DIN 65251:2013-05 Aerospace series - Bolts, with MJ threads, in titanium alloys, strength class 900 MPa and 1 100 MPa - Technical specification
DIN EN 2213:2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bars - D 16 mm - 980 MPa R 1180 MPa; German and English version prEN 2213:2021 ￥365.00 收藏加入购物车
DIN EN ISO 14529-2:2000-08 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 2: Preparation of test specimens and determination of properties (ISO 14529-2:1999); German version EN ISO 14529-2:1999
DIN EN 3524:2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm a 6 mm - 1080 MPa R 1280 MPa; German and English version prEN 3524:2021 ￥365.00 收藏
DIN EN 3526:2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm a 6 mm - 980 MPa R 1180 MPa; German and English version prEN 3526:2021 ￥365.00 收藏
DIN EN 3488:2020 Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Sheets and strips - a 6 mm - 500 MPa R 700 MPa; English version prEN 3488:2020 ￥365.00 收藏加入购物车
DIN EN 2482:2011 Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa R<(Index)m> 1 300 MPa - Bars - D<(Index)e> 100 mm; German and English version EN 2482:2010
DIN EN 3525:2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Plates - 6 mm a 20 mm - 1080 MPa R 1280 MPa; German and English version prEN 3525:2021 ￥365.00 收藏
DIN 65058:2010-03 Aerospace - Bolts and screws in corrosion-resisting steels, with normal tensile strength of 900 MPa and 1100 MPa, for temperatures up to 425 °C - Technical specification; Text in German and English
DIN EN 2278:2014 Aerospace series - Steel X12CrNiMoV12-3 (1.4933) - 900 MPa <= Rm <= 1100 MPa, Bars - De <= 150 mm; German and English version EN 2278:2014
DIN EN 3523:2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bar for machining - D 100 mm - 1080 MPa R 1280 MPa; German and English version prEN 3523:2021 ￥365.00 收藏
DIN EN 2438:2009 Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa R<(Index)m> 1100 MPa - Bars - D<(Index)e> 40 mm; German and English version EN 2438:2008
DIN EN 2205:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa R<(Index)m> 1100 MPa - Bars - D<(Index)e> 40 mm; German and English version EN 2205:2009
DIN EN 2446:2009 Aerospace series - Steel FE-PL1503 (35CrMo4) - 1100 MPa R<(Index)m> 1300 MPa - Bars - D<(Index)e> 25 mm; German and English version EN 2446:2008
DIN EN 2448:2009 Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa R<(Index)m> 1100 MPa - Bars - D<(Index)e> 40 mm; German and English version EN 2448:2008
DIN ISO 8132:2023-03 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series (ISO 8132:2022); Text in German and English / Note: Date of issue 2023-02-10*Intended as replacement for DIN ISO 8...
DIN ISO 8132:2023-11 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series (ISO 8132:2022)
DIN EN 3361:2021 Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Sheets and strips - a 6mm - 1070 MPa R 1220 MPa; English version prEN 3361:2021 ￥365
DIN EN 4904:2023 Aerospace series - Steel 36NiCrMo16 (1.6773) - 1 000 MPa R 1 200 MPa - Bars - 100 mm D 250 mm; German and English version EN 4904:2022 ￥411.00 收藏加入购物车
DIN EN 3762:1994 Aerospace series - Heat resisting alloy FE-PA2601, softened and cold worked; wire for forged fasteners D 15 mm, 1100 MPa R 1300 MPa ￥395.00 收藏加入购物车
DIN EN 2475:2019 Aerospace series - Steel 30CrNiMo8 (1.6580) - Air melted - Hardened and tempered - Bar for machining - D 100 mm - 1 100 MPa R 1 300 MPa; German and English version EN 2475:2018 ￥365.00 收藏
DIN EN 2467:2020 Aerospace series - Steel X2CrNi18-9 (1.4307) - Air melted - Softened - Plates, sheets and strips - 0,4 mm a 20 mm - 520 MPa R 670 MPa; English version prEN 2467:2020 ￥365.00 收藏加
DIN EN 2540:2018 Aerospace series - Steel X7CrNiAl17-7 (1.4568) - Air melted - Solution treated and precipitation hardened - Sheet and strip - a 6 mm - 1 240 MPa R 1 450 MPa; German and English version EN 2540:2018 ￥365.00
DIN ISO 8132:2017 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series (ISO 8132:2014)
DIN ISO 8132:2023 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series (ISO 8132:2022); Text in German and English
DIN EN 4627:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - D e <= 200 mm - 1 150 MPa <= R m <= 1 300 MPa; German and English version EN 4627:2014
DIN EN 2213:2012 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - D<(Index)e> 16 mm - 980 MPa R<(Index)m> 1 180 MPa; German and English version EN 2213:2012
DIN EN 4628:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De 200 mm - 1150 MPa Rm 1300 MPa; German and English version EN 4628:2013
DIN EN 4627:2008 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Forgings - D<(Index)e> 150 mm - 1100 MPa R<(Index)m> 1300 MPa; German and English version EN 4627:2007
DIN EN 3639:2021 Aerospace series - Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) - Softened and cold worked - Wires for forged fasteners - D ≤ 15 mm - 900 MPa ≤ Rm ≤ 1 100 MPa; German and English version EN 3639:2021
DIN EN 2481:2011 Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa R<(Index)m> 1 400 MPa - Forgings - D<(Index)e> 75 mm; German and English version EN 2481:2010
DIN EN 2483:2011 Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa R<(Index)m> 1 300 MPa - Forgings - D<(Index)e> 100 mm; German and English version EN 2483:2010
DIN EN 4825:2020 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - D 150 mm - 900 MPa R 1100 MPa; German and English version FprEN 4825:2020 ￥344.00
DIN EN 4721:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De <= 200 mm - 900 MPa <= Rm <= 1050 MPa; German and English version EN 4721:2014
DIN EN 4720:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De <= 200 mm - 1150 MPa <= Rm <= 1300 MPa; German and English version EN 4720:2014
DIN EN 2952:2019 Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked - Bar for forged fasteners - D 50 mm - 1 270 MPa R 1 550 MPa; German and English version EN 2952:2019 ￥365.00
DIN EN 4244:2020 Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted - Hardened and tempered - Bars - a or D 200 mm - 1 000 MPa R 1 140 MPa; German and English version EN 4244:2020 ￥411.00
DIN EN 3479:2021 Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a 20 mm - 1070 MPa Rm 1220 MPa; English version prEN 3479:2021 ￥351.
DIN EN 3355:2012 Aerospace series - Titanium alloy TI-P64001 (Ti-6AI-4V) - Annealed - Extruded section - D<(Index)e> 150 mm - 900 MPa R<(Index)m> 1 160 MPa; German and English version EN 3355:2012
DIN EN 4628:2008 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Bar - D<(Index)e> 150 mm - 1100 MPa R<(Index)m> 1300 MPa; German and English version EN 4628:2007
DIN EN 3479:2023 Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a 20 mm - 1 070 MPa R 1 220 MPa; German and English version EN 3479:2022
DIN EN 2460:2009 Aerospace series - Steel FE-PM1901 (X12CrNi13) - 600 MPa R<(Index)m> 800 MPa - Bars - D<(Index)e> 70 mm; German and English version EN 2460:2009
DIN EN 2252:2012 Aerospace series - Steel FE-PL1505 (15CrMoV6) - 1 080 MPa R<(Index)m> 1 250 MPa - Forgings - D<(Index)e> 100 mm; German and English version EN 2252:2012
DIN EN 4528:2009 Aerospace series - Steel FE-PA3903 (X10CrNi18-8) - Cold rolled - Strip for springs - a 3 mm - 1 250 MPa R<(Index)m> 1 640 MPa; German and English version EN 4528:2009
DIN EN 3470:2019 Aerospace series - Steel FE-PM1503 (X3CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D 150 mm - 1 200 MPa R 1 400 MPa; German and English version EN 3470:2019
DIN EN 4884:2023 Aerospace series - Steel X3CrNiMoAl (1.4534) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D 200 mm - 1 200 MPa Rm 1 350 MPa; German and English version EN 4884:2022
DIN EN 4263:2014 Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D <= 200 mm - 690 MPa <= R m <= 960 MPa; German and English version EN 4263:2013
DIN EN 4262:2014 Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D <= 200 mm - 690 MPa <= R m <= 880 MPa; German and English version EN 4262:2013
DIN EN 3762:2023 Aerospace series - Heat-resisting alloy X6NiCrTiMnMoV26-15 (1.4944) - Softened and cold worked - Wire for forged fasteners - D 15 mm - 1 100 MPa R 1 300 MPa; German and English version EN 3762:2022 ￥411.00

SAE - SAE International, mp and mpa

SAE MA3376C-2018 Bolts & Screws@ UNS G87400 Tensile Strength 860 MPa & 1000 MPa Procurement Specification@ Metric
SAE MA1943B-2018 Nuts@ Self-Locking@ UNS N07001 730 °C@ 1100 MPa@ and 1210 MPa Procurement Specification for@ Metric
SAE AMS6386B-1974 Steel Sheet and Plate Low Alloy@ Heat Treated 90@000 psi (621 MPa) and 100@000 psi (690 MPa) Yield Strength
SAE AMS6386D-2016 Steel Sheet and Plate Low Alloy@ Heat Treated 90@000 psi (621 MPa) and 100@000 psi (690 MPa) Yield Strength
SAE AMS4900D-1972 TITANIUM SHEET@ STRIP@ AND PLATE Annealed 55@000 psi (379 Mpa) Yield
SAE AMS4901F-1977 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (483 Mpa) Yield Strength
SAE AMS4900E-1977 TITANIUM SHEET@ STRIP@ AND PLATE Annealed 55@000 psi (379 Mpa) Yield Strength
SAE AMS4901E-1972 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (483 Mpa) Yield Strength
SAE AMS4921D-1977 TITANIUM BARS@ FORGINGS@ AND RINGS Annealed@ 70@000 psi (483 MPa) Yield Strength
SAE AMS4926D-1972 TITANIUM ALLOY BARS AND RINGS 5Al - 2.5Sn Annealed@ 110@000 psi (758 MPa) Yield
SAE MA3376A-1986 Bolts & Screws@ UNS G87400 860 MPa@ MJ Thread@ Procurement Specification for@ Metric
SAE AMS4901R-2010 Titanium Sheet@ Strip@ and Plate Commercially Pure Annealed@ 70.0 ksi (485 MPa) (UNS R50700)
SAE AMS4901M-1991 Titanium Sheet@ Strip@ and Plate Commercially Pure Annealed@ 70.0 ksi (485 MPa) (UNS R50700)
SAE MA3378B-1990 Bolts and Screws@ UNS N07001 730 Degrees C@ 1210 MPa Procurement Specification for@ Metric
SAE AMS4921C-1976 Titanium Bars@ Wire@ Forgings@ and Rings Annealed@ 70@000 psi (483 MPa) Yield Strength
SAE AMS4901K-1986 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (485 Mpa) Yield Strength (UNS R50700)
SAE AMS4900G-1984 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 55@000 psi (380 Mpa) Yield Strength (UNS R50550)
SAE AMS4902D-1986 TITANIUM SHEET@ STRIP@ AND PLATE Annealed 40@000 psi (275 MPa) Yield Strength (UNS R50400)
SAE AMS4901J-1984 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (485 Mpa) Yield Strength (UNS R50700)
SAE AMS4901H-1978 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (483 Mpa) Yield Strength (UNS R50700)
SAE AMS4900H-1986 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 55@000 psi (380 Mpa) Yield Strength (UNS R50550)
SAE AMS4901L-1986 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (485 Mpa) Yield Strength (UNS R50700)
SAE AMS4921F-1985 Titanium Bars@ Wire@ Forgings@ and Rings Annealed@ 70@000 psi (483 MPa) Yield Strength
SAE AMS4901G-1977 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 70@000 psi (483 Mpa) Yield Strength (UNS R50700)
SAE AMS4921E-1979 Titanium Bars@ Forgings@ and Rings Annealed@ 70@000 psi (483 MPa) Yield Strength (UNS R50700)
SAE AMS4900J-1986 TITANIUM SHEET@ STRIP@ AND PLATE Annealed@ 55@000 psi (380 Mpa) Yield Strength (UNS R50550)
SAE AMS4900F-1977 TITANIUM SHEET@ STRIP@ AND PLATE Annealed 55@000 psi (379 Mpa) Yield Strength (UNS R50550)
SAE AMS4902C-1980 TITANIUM SHEET@ STRIP@ AND PLATE Annealed 40@000 psi (276 MPa) Yield Strength (UNS R50400)
SAE AMS4926E-1976 TITANIUM ALLOY BARS AND RINGS 5Al - 2.5Sn Annealed@ 110@000 psi (758 MPa) Yield Strength
SAE AMS4928G-1972 TITANIUM ALLOY BARS AND FORGINGS 6Al - 4V Annealed@ 120@000 psi (827 MPa) Yield
SAE AMS4926F-1977 Titanium Alloy Bars and Rings 5A1 - 2.5Sn Annealed@ 110@000 psa (758 MPa) Yield Strength
SAE AMS4928H-1977 Titanium Alloy Bars and Forgings 5Al - 4V Annealed@ 120@000 psi (827 MPa) Yield
SAE AMS4921G-1991 Titanium Bars@ Wire@ Forgings@ and Rings Commercially Pure 70.0 ksi (483 MPa) Yield Strength
SAE AMS4902E-1986 TITANIUM SHEET@ STRIP AND PLATE Annealed 40@000 psi (275 MPa) Yield Strength (UNS R50400)
SAE AMS4900K-1991 Titanium Sheet@ Strip@ and Plate Commercially Pure Annealed@ 55.0 ksi (379 MPa) Yield Strength
SAE AMS4921H-2002 Titanium Bars@ Wire@ Forgings@ and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700)
SAE AMS4921N-2016 Titanium Bars@ Wire@ Forgings@ and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength (UNS R50700)
SAE MA1568A-2018 Nut@ Self Locking - UNS S66286@ 425°C & 650°C@ 1100 MPa@ MJ Thread@ Procurement Specification For@ Metric
SAE AMS4908F-1994 Titanium Alloy@ Sheet and Strip 8Mn Annealed@ 110 ksi (758 MPa) Yield Strength (UNS R56080)
SAE AMS4926G-1983 Titanium Alloy Bars and Rings 5A1 - 2.5Sn Annealed@ 110@000 psi (760 MPa) Yield Strength (UNS R54520)
SAE AMS4926H-1988 Titanium Alloy Bars and Rings 5Al - 2.5Sn Annealed@ 110@000 psi (760 MPa) Yield Strength (UNS R54520)
SAE AMS6317F-1991 Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated@ 125 ksi (862 MPa) Tensile Strength
SAE AMS4908G-2003 Titanium Alloy@ Sheet and Strip 8Mn Annealed@ 110 ksi (758 MPa) Yield Strength (UNS R56080)
SAE AMS6472C-1991 Steel Bars and Forgings@ Nitriding 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) Hardened and Tempered@ 112 ksi (772 MPa) Tensile Strength
SAE AMS4908E-1988 TITANIUM ALLOY SHEET AND STRIP 8Mn Annealed@ 110@000 psi (760 Mpa) Yield Strength (UNS R56080)
SAE AMS4908D-1981 TITANIUM ALLOY SHEET AND STRIP 8Mn Annealed@ 110@000 psi (760 Mpa) Yield Strength (UNS R56080)
SAE AMS4902F-1991 Titanium Sheet@ Strip@ and Plate Commercially- Pure Annealed 40.0 ksi (276 MPa) Yield Strength (UNS R50400)
SAE AMS6317D-1978 STEEL BARS AND FORGINGS 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated@ 125@ 000 psi (862 MPa) Tensile Strength
SAE AMS6317E-1986 STEEL BARS AND FORGINGS 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated@ 125@ 000 psi (860 MPa) Tensile Strength
SAE AMS5906-1992 Steel Sheet and Strip@ Corrosion Resistant 18Cr - 9.0Ni (SAE 30302) Cold Rolled@ 185 ksi (1276 MPa) Tensile (UNS S30200)
SAE AMS5912-1992 Steel Sheet and Strip@ Corrosion Resistant 19Cr - 9.2Ni (SAE 30304) Cold Rolled@ 175 ksi (1207 MPa) Tensile Strength
SAE AMS5911-1992 Steel Sheet and Strip@ Corrosion Resistant 19Cr - 9.2Ni (SAE 30304) Cold Rolled@ 150 ksi (1034 MPa) Tensile Strength
SAE AMS5913-1992 Steel Sheet and Strip@ Corrosion Resistant 19Cr - 9.2Ni (SAE 30304) Cold Rolled@ 185 ksi (1276 MPa) Tensile Strength
SAE MA3377C-2018 Bolts and Screws@ Nickel Alloy UNS N07718@ Tensile Strength 1275 MPa Procurement Specification@ Metric

International Organization for Standardization (ISO), mp and mpa

ISO 9609:2016 Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature) /120 degrees C, 450 MPa (at ambient temperature) /235 degrees C, 600 MPa (at ambient temperature) /425 degrees C, 9
ISO 9609:1996 Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 °C, 450 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/425 °C, 900 MPa (at ambient tempe
ISO 9199:1998 Aerospace - Nuts, bihexagonal, self-locking, MJ threads, classifications: 1100 MPa (at ambient temperature)/425 °C, 1100 MPa (at ambient temperature)/650 °C, 1210 MPa (at ambient temperature)/425 °C, 1210 MPa (at ambient temperature)/730 °C, 1550 MPa (at
ISO 9618:2016 Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 degrees C, 450 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperature)/425
ISO 9618:1996 Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 °C, 450 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/425 °C, 900 MPa (
ISO 10096:1997 Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, reduced across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/425 °C, 600 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/315 °C, 600 MPa
ISO 8135:1999 Hydraulic fluid power - Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series - Tolerances
ISO 6150:1988 Pneumatic fluid power; cylindrical quick-action couplings for maximum working pressures of 10 bar, 16 bar and 25 bar (1 MPa, 1,6 MPa and 2,5 MPa); plug connecting dimensions, specifications, application guidelines and testing
ISO 14529-2:1999 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 2: Preparation of test specimens and determination of properties
ISO 12278:1999 Aerospace - Nuts, barrel, self-locking, floating, self-aligning, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/235 °C, 1250 MPa (at ambient temperature)/235 °C and 1550 MPa (at ambient tempera
ISO 8132:2006 Hydraulic fluid power - Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series - Mounting dimensions for accessories
ISO 8132:1986 Hydraulic fluid power; Single rod cylinders, 160 bar (16 MPa) medium and 250 bar (25 MPa) series; Mounting dimensions for accessories
ISO 8132:2022 Hydraulic fluid power — Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
ISO 8538:1999 Aerospace - Nuts, hexagonal, self-locking, with counterbore and captive washer, 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
ISO 12277:2000 Aerospace - Gang channel, self-locking, floating, standard series, with counterbore, classifications: 1100 MPa (at ambient temperature)/120 °C, 1100 MPa (at ambient temperature)/235 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions
ISO 8132:2014 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
ISO 3209:1998 Aerospace - 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
ISO 3223:1998 Aerospace - Nuts, anchor, self-locking, fixed, 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
ISO 3224:1998 Aerospace - Nuts, anchor, self-locking, floating, single 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
ISO 3209:2016 Aerospace - Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)/425
ISO 3221:1998 Aerospace - Nuts, anchor, self-locking, fixed, 90° corner, 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
ISO 12273:2010 Aerospace - 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 and 900 MPa (at ambient temperature)/425 °C - Dimensions
ISO 12272:1998 Aerospace - Nuts, anchor, self-locking, floating, two lug, with incremental counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C and 900 MPa (at ambient temperature)/425 °C - Dimen
ISO 3225:1998 Aerospace - Nuts, anchor, self-locking, fixed, two lug, reduced series, 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 - D
ISO 3191:1998 Aerospace - Nuts, anchor, self-locking, fixed, single lug, reduced series, 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
ISO 7332:1998 Aerospace - Nuts, anchor, self-locking, floating, two lug, reduced series, 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
ISO 9156:1998 Aerospace - Nuts, anchor, self-locking, fixed, 90° corner, reduced series, 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
ISO 3222:1998 Aerospace - Nuts, anchor, self-locking, fixed, closed corner, reduced series, 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

Danish Standards Foundation, mp and mpa

DS/EN ISO 14529-1:2000 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 1: Designation and basis for specifications
DS/EN ISO 14529-2:2000 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 2: Preparation of test specimens and determination of properties
DS/EN 2209:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa <= Rm <= 1 100 MPa - Sheets, strips and plates - 0,5 mm <= a <= 20 mm
DS/EN 4631:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De <= 200 mm - 900 MPa <= Rm <= 1 050 MPa
DS/EN 3491:2007 Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Forgings - De <= 100 mm - 900 MPa <= Rm <= 1 100 MPa
DS/EN 4098:2007 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Remelted, hardened and tempered, forgings De <= 50 mm, 1 250 MPa <= Rm <= 1 400 MPa
DS/EN 3524:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 2 mm <= a <= 6 mm - 1080 MPa <= Rm <= 1280 MPa
DS/EN 3526:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm <= a <= 6 mm - 980 MPa <= Rm <= 1180 MPa
DS/EN 3488:2007 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Sheet and strip - a <= 6 mm - 500 MPa <= Rm <= 700 MPa
DS/EN 3507:2007 Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Forgings - De <= 100 mm - 930 MPa <= Rm <= 1 080 MPa
DS/EN 2213:2012 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - De <= 16 mm - 980 MPa <= Rm <= 1 180 MPa
DS/EN 3525:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Plate - 6 mm < a <= 20 mm - 1080 MPa <= Rm <= 1280 MPa
DS/EN 4628:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De <= 200 mm - 1 150 MPa <= Rm <= 1 300 MPa
DS/EN 3523:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bar for machining - De <= 100 mm - 1080 MPa <= Rm <= 1280 MPa
DS/EN 4627:2008 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Forgings - De <= 150 mm - 1 100 MPa <= Rm <= 1 300 MPa
DS/EN 4825:2021 Aerospace series – Steel X12CrNiMoV12-3 (1.4938) – Air melted and consumable electrode remelted – Hardened and tempered – Bars – De ≤ 150 mm – 900 MPa ≤ Rm ≤ 1 100 MPa
DS/EN 3490:2007 Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Bar for machining - De <= 200 mm - 900 MPa <= Rm <= 1100 MPa
DS/EN 4642:2009 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Sheet and plate - 0,6 mm <= a <= 50 mm - 900 MPa <= Rm <= 1 050 MPa
DS/EN 2467:2007 Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Air melted - Softened - Plate, sheet and strip - 0,4 mm <= a <= 20 mm - 520 MPa <= Rm <= 670 MPa
DS/EN 3361:2007 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a <= 6mm, 1 070 MPa <= Rm <= 1 220 MPa
DS/EN 3639:2021 Aerospace series – Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) – Softened and cold worked – Wires for forged fasteners – D ≤ 15 mm – 900 MPa ≤ Rm ≤ 1 100 MPa
DS/EN 3972:2007 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Hardened and tempered - Bar for machining - De <= 50 mm - 1 250 MPa <= Rm <= 1 400 MPa
DS/EN 3479:2007 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a <= 20 mm - 1070 MPa <= Rm <= 1220 MPa
DS/EN 3120:2012 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm <= D <= 51 mm - 690 MPa <= Rm <= 1 030 MPa
DS/EN 3531:2007 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Sheet and strip - a <= 6 mm - 1 750 MPa <= Rm <= 2 000 MPa
DS/EN 3528:2013 Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D <= 150 mm - 1 750 MPa <= Rm <= 2 000 MPa
DS/EN 3532:2007 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Plate - 6 mm < a <= 40 mm - 1750 MPa <= Rm <= 2000 MPa
DS/EN 3529:2010 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Forgings - a or D <= 150 mm - 1 750 MPa <= Rm <= 2 000 MPa

ES-UNE, mp and mpa

UNE-EN ISO 14529-1:2000 PLASTICS - MELAMINE/PHENOLIC POWDER MOULDING COMPOUNDS (MP-PMCs) - PART 1: DESIGNATION SYSTEM AND BASIS FOR SPECIFICATIONS (ISO 14529-1:1999)
UNE-EN 2209:2008 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa <= Rm <= 1 100 MPa - Sheets, strips and plates - 0,5 mm <= a <= 20 mm (Endorsed by AENOR in January of 2009.)
UNE-EN 4098:2007 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Remelted, hardened and tempered, forgings De <= 50 mm, 1 250 MPa <= Rm <= 1 400 MPa (Endorsed by AENOR in November of 2007.)
UNE-EN ISO 14529-2:2000 PLASTICS - MELAMINE/PHENOLIC POWDER MOULDING COMPOUNDS (MP-PMCs) - PART 2: PREPARATION OF TEST SPECIMENS AND DETERMINATION OF PROPERTIES. (ISO 14529-2:1999)
UNE-EN 3524:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 2 mm = a = 6 mm - 1 080 MPa = Rm = 1 280 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 4890:2022 Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered - Sheets and plates - 0,3 mm = a = 50 mm - 900 MPa = Rm = 1 050 MPa
UNE-EN 3507:2006 Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Forgings - De = 100 mm - 930 MPa = Rm = 1 080 MPa (Endorsed by AENOR in April of 2007.)
UNE-EN 2213:2012 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - De <= 16 mm - 980 MPa <= Rm <= 1 180 MPa (Endorsed by AENOR in April of 2012.)
UNE-EN 4630:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De <= 200 mm - 900 MPa <= Rm <= 1 050 MPa (Endorsed by AENOR in December of 2014.)
UNE-EN 3491:2006 Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Forgings - De = 100 mm - 900 MPa = Rm = 1 100 MPa (Endorsed by AENOR in April of 2007.)
UNE-EN 3488:2007 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Sheet and strip - a <= 6 mm - 500 MPa <= Rm <= 700 MPa (Endorsed by AENOR in November of 2007.)
UNE-EN 4631:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De <= 200 mm - 900 MPa <= Rm <= 1 050 MPa (Endorsed by AENOR in April of 2013.)
UNE-EN 4627:2022 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De = 200 mm - 1 150 MPa = Rm = 1 300 MPa
UNE-EN 4628:2022 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bars - De = 200 mm - 1 150 MPa = Rm = 1 300 MPa
UNE-EN 2475:2018 Aerospace series - Steel 30CrNiMo8 (1.6580) - Air melted - Hardened and tempered - Bar for machining - De = 100 mm - 1 100 MPa = Rm = 1 300 MPa
UNE-EN 3526:2007 Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm = a = 6 mm - 980 MPa = Rm = 1 180 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 4642:2009 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Sheet and plate - 0,6 mm <= a <= 50 mm - 900 MPa <= Rm <= 1 050 MPa (Endorsed by AENOR in March of 2009.)
UNE-EN 4825:2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De = 150 mm - 900 MPa = Rm = 1 100 MPa
UNE-EN 4721:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De <= 200 mm - 900 MPa <= Rm <= 1 050 MPa (Endorsed by AENOR in December of 2014.)
UNE-EN 4720:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De <= 200 mm - 1 150 MPa <= Rm <= 1 300 MPa (Endorsed by AENOR in December of 2014.)
UNE-EN 2540:2018 Aerospace series - Steel X7CrNiAl17-7 (1.4568) - Air melted - Solution treated and precipitation hardened - Sheet and strip - a = 6 mm - 1 240 MPa = Rm = 1 450 MPa
UNE-EN 2467:2007 Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Air melted - Softened - Plate, sheet and strip - 0,4 mm <= a <= 20 mm - 520 MPa <= Rm <= 670 MPa (Endorsed by AENOR in November of 2007.)
UNE-EN 3761:2020 Aerospace series - Heat resisting alloy FE-PA2601 - Softened and cold worked - Bar for forged fasteners - D = 50 mm - 1 100 MPa = Rm = 1 300 MPa
UNE-EN 3972:2006 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Hardened and tempered - Bar for machining - De = 50 mm - 1 250 MPa = Rm = 1 400 MPa (Endorsed by AENOR in April of 2007.)
UNE-EN 3639:2021 Aerospace series - Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) - Softened and cold worked - Wires for forged fasteners - D = 15 mm - 900 MPa = Rm = 1 100 MPa
UNE-EN 3361:2007 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a <= 6mm, 1 070 MPa <= Rm <= 1 220 MPa (Endorsed by AENOR in November of 2007.)
UNE-EN 3523:2007 Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bar for machining - De = 100 mm - 1 080 MPa = Rm = 1 280 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 3525:2007 Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Plate. 6 mm < a = 20 mm - 1 080 MPa = Rm = 1 280 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 2952:2019 Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked - Bar for forged fasteners - D <= 50 mm - 1 270 MPa <= Rm <= 1 550 MPa (Endorsed by Asociación Española de Normalización in May of 2019.)
UNE-EN 3762:2022 Aerospace series - Heat-resisting alloy X6NiCrTiMnMoV26-15 (1.4944) - Softened and cold worked - Wire for forged fasteners - D = 15 mm - 1 100 MPa = Rm = 1 300 MPa
UNE-EN 3666:2020 Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked - Bar for forged fasteners - D <= 50 mm - 1 550 MPa <= Rm <= 1 830 MPa (Endorsed by Asociación Española de Normalización in February of 2020.)
UNE-EN 4244:2020 Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted - Hardened and tempered - Bars - a or D = 200 mm - 1 000 MPa = Rm = 1 140 MPa
UNE-EN 3490:2007 Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Bar for machining - De = 200 mm - 900 MPa = Rm = 1 100 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 3120:2012 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm <= D <= 51 mm - 690 MPa <= Rm <= 1 030 MPa (Endorsed by AENOR in March of 2012.)
UNE-EN 3531:2007 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Sheet and strip - a = 6 mm - 1 750 MPa = Rm = 2 000 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 3532:2007 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Plate - 6 mm < a = 40 mm - 1 750 MPa = Rm = 2 000 MPa (Endorsed by AENOR in May of 2007.)
UNE-EN 3470:2019 Aerospace series - Steel FE-PM1503 (X3CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D = 150 mm - 1 200 MPa = Rm = 1 400 MPa
UNE-EN 4884:2022 Aerospace series - Steel X3CrNiMoAl (1.4534) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D = 200 mm - 1 200 MPa = Rm = 1 350 MPa
UNE-EN 3528:2013 Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D <= 150 mm - 1 750 MPa <= Rm <= 2 000 MPa (Endorsed by AENOR in February of 2013.)
UNE-EN 3529:2010 Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Forgings - a or D = 150 mm - 1 750 MPa = Rm = 2 000 MPa (Endorsed by AENOR in April of 2010.)
UNE-EN 3357:2019 Aerospace series - Steel FE-PM1503 (X3CrNiMoAl 13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D = 150 mm - 1 200 MPa = Rm = 1 400 MPa

Association Francaise de Normalisation, mp and mpa

NF EN ISO 14529-1:2000 Plastiques - Poudres à mouler à base de mélamine/phénol (MP-PMC) - Partie 1 : système de désignation et base de spécification
NF E49-053:2005 Pneumatic fluid power - Cylindrical quick-action couplings for maximum working pressures of 10 bar, 16 bar and 25 bar (1 MPa, 1,6 MPa and 2,5 MPa) - Plug connecting dimensions, specifications, application guidelines and testing.
NF ISO 6150:2019 Transmissions pneumatiques - Raccords rapides cylindriques pour pressions maximales d'utilisation 1 MPa, 1,6 MPa et 2,5 MPa (10 bar, 16 bar et 25 bar) - Dimensions de raccordement de la partie mâle, spécifications, conseils d'utilisation et essais
NF EN ISO 14529-2:2000 Plastiques - Poudres à mouler à base de mélamine/phénol (MP-PMC) - Partie 2 : préparation des éprouvettes et détermination des propriétés
NF E49-053*NF ISO 6150:2019 Pneumatic fluid power - Cylindrical quick-action couplings for maximum working pressures of 1 MPa, 1,6 Mpa, and 2,5 MPa (10 bar, 16 bar and 25 bar) - Plug connecting dimensions, specifications, application guidelines and testing
NF E48-501:2006 Hydraulic fluid power - Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series - Mounting dimensions for accessories.
NF L10-545*NF EN 4628:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De < or = 200 mm - 1 150 MPa < or = Rm < or = 1 300 MPa
NF L10-548*NF EN 4631:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De < or = 200 mm - 900 MPa < or = Rm < or = 1 050 MPa
NF E48-501:2015 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
NF E48-501*NF ISO 8132:2022 Hydraulic fluid power - Mounting dimensions for accessories for single rod cylinders, 16 MPa (160 bar) medium and 25 MPa (250 bar) series
PR EN 3441:1994 Aerospace series. Titanium ti-P99001. Annealed. Sheet and strip, hot rolled, a inferior or equal to 6 mm. 290 MPa inferior or equal to 420 MPa.
NF L10-598*NF EN 4720:2015 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De < or = 200 mm - 1 150 MPa < or = Rm < or = 1 300 MPa
NF L10-599*NF EN 4721:2015 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De < or = 200 mm - 900 MPa < or = RM < or = 1 050 MPa
NF EN 2451:2019 Série aérospatiale - Acier 31Ni10 - 1 230 MPa inférieur ou égal à Rm inférieur ou égal à 1 420 MPa - Pièces forgées et matricées - De inférieur ou égal à 40 mm
NF L14-641*NF EN 3120:2012 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm < or = D < or = 51 mm - 690 MPa < or = Rm < or = 1 030 MPa
NF L22-564:1985 Gang channel self-locking nuts classification 900 MPa/120 degrees C and 235 degrees C. ISO thread.
NF L22-551:1985 Self-locking anchor nuts, two lugs classification 900 MPa/235 degrees C and 425 degrees C. ISO thread.
PR EN 3443:1994 Aerospace series. Titanium ti-P99003. Annealed. Sheet and strip, hot rolled, a inferior or equal to 6 mm. 570 MPa inferior or equal to rm inferior or equal to 730 MPa.
PR EN 3499:1994 Aerospace series. Titanium ti-P99003. Annealed. Sheet and strip, cold rolled, a inferior or equal to 6 mm. 570 MPa inferior or equal to rm inferior or equal to 730 MPa.
PR EN 3498:1994 Aerospace series. Titanium ti-P99002. Annealed. Sheet and strip, cold rolled, a inferior or equal to 6 mm. 390 MPa inferior or equal to rm inferior or equal to 540 MPa.
PR EN 3442:1994 Aerospace series. Titanium ti-P99002. Annealed. Sheet and strip, hot rolled, a inferior or equal to 6 mm. 390 MPa inferior or equal to rm inferior or equal to 540 MPa.
NF L10-570*NF EN 4642:2009 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Sheet and plate - 0,6 mm < or = a < or = 50 mm - 900 MPa < or = Rm < or = 1 050 MPa.
PR EN 3497:1994 Aerospace series. Titanium ti-P99001. Annealed. Sheet and strip, cold rolled a inferior or equal to 6 mm. 290 MPa inferior or equal to rm inferior or equal to 420 MPa.
NF L10-719*NF EN 2952:2019 Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked - Bar for forged fasteners - D< or = 50 mm - 1 270 MPa < or = Rm < or = 1 550 MPa
NF L10-511*NF EN 3528:2013 Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D < ou = 150 mm - 1 750 MPa < or = Rm < or = 2 000 MPa
NF L22-553:1985 Self-locking anchor nuts, 90 degrees corner classification 900 MPa/235 degrees C and 425 degrees C. ISO thread.
NF E49-053:1989 Pneumatic fluid power. Cylindrical quick-action couplings for maximum working pressures of 16 bar and 25 bar (1,6 MPa and 2,5 MPa). Plug connecting dimensions, specifications, application guidelines and testing.
NF L10-547*NF EN 4627:2015 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De < ou = 200 mm - Rm greater than or equal to 1 150 MPa and less than or equal to 1 300 MPa
NF L11-036*NF EN 4825:2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De less than or equal to 150 mm - 900 MPa less than or equal to Rm less than or equal to 1 100 MPa
NF L10-723*NF EN 2540:2018 Aerospace series - Steel X7CrNiAl17-7 (1.4568) - Air melted - Solution treated and precipitation hardened - Sheet and strip - a less than or equal to 6 mm - 1 240 MPa less than or equal to Rm less than or equal to 1 450 MPa
NF L11-025*NF EN 3761:2020 Aerospace series - Heat resisting alloy FE-PA2601 - Softened and cold worked - Bar for forged fasteners - D less than or = at 50 mm - 1 100 MPa less than or = at Rm less than or = at 1 300 MPa
NF L22-561:1985 Self-locking anchor nuts, floating, two lugs classification 900 MPa/235 degrees C and 425 degrees C. ISO thread.
NF L22-552:1985 Self-locking anchor nuts, single lug with two holes. Classification 900 MPa/235 degrees C and 425 degrees C. ISO thread.

Korean Agency for Technology and Standards (KATS), mp and mpa

KS B ISO 8135:2004 Hydraulic fluid power-Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa(250 bar) series-Tolerances
KS B ISO 8135:2013 Hydraulic fluid power－Single rod cylinders, 16 MPa (160 bar) medium and 25 MPa(250 bar) series－Tolerances
KS M ISO 14529-2:2006 Plastics-Melamine/phenolic powder moulding compounds(MP-PMCs)-Part 2:Preparation of test specimens and determination of properties
KS M ISO 14529-1-2006(2016) Plastics－Melamine/phenolic powder moulding compounds(MP－PMCs)－Part 1：Designation system and basis for specifications
KS M ISO 14529-2-2006(2021) Plastics－Melamine/phenolic powder moulding compounds(MP－PMCs)－Part 2：Preparation of test specimens and determination of properties
KS M ISO 14529-1-2006(2021) Plastics－Melamine/phenolic powder moulding compounds(MP－PMCs)－Part 1：Designation system and basis for specifications
KS M ISO 14529-2-2006(2016) Plastics－Melamine/phenolic powder moulding compounds(MP－PMCs)－Part 2：Preparation of test specimens and determination of properties
KS B ISO 6164-2004(2009) Hydraulic fluid power－Four-screw, one-piece square-flange connections for use at pressures of 25 MPa and 40 MPa
KS W ISO 8538:2020 Aerospace — Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 °C, 1 100 MPa (at ambient temperature)/315 °C a
KS W ISO 9156:2020 Aerospace — Nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, with MJ threads, classifications:1 100 MPa (at ambient temperature)/235 °C,1 100 MPa (at ambient temperatur

Aerospace, Security and Defence Industries Association of Europe (ASD), mp and mpa

ASD-STAN PREN 2440-2010 Aerospace series Steel FE-PL711 1250 MPa = Rm = 1450 MPa Bars and wires De = 16 mm Edition 2
ASD-STAN PREN 2445-2010 Aerospace series Steel FE-PL8201 (41NiCrMo2) Air melted Hardened and temperedForgings De = 45 mm 900 MPa = Rm = 1100 Mpa Edition P2
ASD-STAN PREN 3518-2010 Aerospace series Steel FE-PL2105 Air melted Hardened and tempered Forgings - De = 150 mm 1080 MPa = rm = 1280 MPa Edition P3
ASD-STAN PREN 3477-2010 Aerospace series Steel FE-PM3503 (X7CrNiMo15-7-3) Air melted Solution treated and precipitation treated Plate - 6 mm< a = 15 mm 1 310 MPa = Rm = 1 550 MPa Edition P3

ASD-STAN - Aerospace and Defence Industries Association of Europe - Standardization, mp and mpa

PREN 2440-2010 Aerospace series Steel FE-PL711 1250 MPa ≤ Rm ≤ 1450 MPa Bars and wires De ≤ 16 mm (Edition 2)
PREN 3518-2010 Aerospace series Steel FE-PL2105 Air melted Hardened and tempered Forgings - De ≤ 150 mm 1080 MPa ≤ rm ≤ 1280 MPa (Edition P3)
PREN 2305-1980 Nickel Base Alloy NI-P11 540 MPa Less Than or Equal to Rm Less Than or Equal to 620 MPa Bars and Wires for Rivets Aerospace Series (Edition 1)
PREN 2305-1999 Nickel Base Alloy NI-P11 540 MPa Less Than or Equal to Rm Less Than or Equal to 620 MPa Bars and Wires for Rivets Aerospace Series (Edition 2)
PREN 2276-1979 Steel FE-PA95 1750 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Sheet and Plate a Less Than or Equal to 40 mm Aerospace Series (Edition 1)
PREN 2440-1981 Steel FE-PL711 1250 MPa Less Than or Equal to Rm Less Than or Equal to 1450 MPa Bars and Wires De Less Than or Equal to 16 mm Aerospace Series (Edition 1)
PREN 2444-1981 Steel FE-PL711 900 MPa Less Than or Equal to Rm Less Than or Equal to 1100 MPa Bars and Wires De Less Than or Equal to 45 mm Aerospace Series (Edition 1)
PREN 2442-1981 Steel FE-PL711 1100 MPa Less Than or Equal to Rm Less Than or Equal to 1300 MPa Bars and Wires De Less Than or Equal to 25 mm Aerospace Series (Edition 1)
PREN 2273-1979 Steel FE-PM13 S 1800 MPa Less Than or Equal to Rm Less Than or Equal to 2000 MPa Sheet and Plate a Less Than or Equal to 30 mm Aerospace Series (Edition 1)
PREN 3477-2010 Aerospace series Steel FE-PM3503 (X7CrNiMo15-7-3) Air melted Solution treated and precipitation treated Plate - 6 mm < a ≤ 15 mm 1 310 MPa ≤ Rm ≤ 1 550 MPa (Edition P3)
PREN 2252-1977 Steel FE-PL52 S 1080 MPa Less Than or Equal to Rm Less Than or Equal to 1250 MPa Hand and Die Forgings De Less Than or Equal to 100 mm Aerospace Series (Edition 1)
PREN 3442-1993 Aerospace Series Titanium TI-P99002 Annealed Sheet and Strip@ Hot Rolled a Less Than or Equal to 6 mm 390 MPa Less Than or Equal to Rm Less Than or Equal to MPa (Edition P 2)
PREN 3443-1993 Aerospace Series Titanium TI-P99003 Annealed Sheet and Strip@ Hot Rolled a Less Than or Equal to 6 mm 570 MPa Less Than or Equal to Rm Less Than or Equal to MPa (Edition P 2)
PREN 4627-2006 Aerospace series Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forgings De < or = to 150 mm 1 100 MPa < or = to Rm < or = to 1 300 MPa (Edition P 1)
PREN 3441-1993 Aerospace Series Titanium TI-P99001 Annealed Sheet and Strip@ Hot Rolled a Less Than or Equal to 6 mm 290 MPa Less Than or Equal to Rm Less Than or Equal to 420 MPa (Edition P 2)
PREN 3497-1993 Aerospace Series Titanium TI-P99001 Annealed Sheet and Strip@ Cold Rolled a Less Than or Equal to 6 mm 290 MPa Less Than or Equal to Rm Less Than or Equal to 420 MPa (Edition P 2)
PREN 3499-1993 Aerospace Series Titanium TI-P99003 Annealed Sheet and Strip@ Cold Rolled a Less Than or Equal to 6 mm 570 MPa Less Than or Equal to Rm Less Than or Equal to 730 MPa (Edition P 2)
PREN 3498-1993 Aerospace Series Titanium TI-P99002 Annealed Sheet and Strip@ Cold Rolled a Less Than or Equal to 6 mm 390 MPa Less Than or Equal to Rm Less Than or Equal to 540 MPa (Edition P 2)
PREN 4628-2006 Aerospace series Steel FE-PM 3504 (X4CrNiMo16-5-1) Air melted Hardened and tempered Forgings Bar De < or = to 150 mm 1 100 MPa < or = to Rm < or = to 1 300 MPa (Edition P 1)

AT-ON, mp and mpa

OENORM EN 4631-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bars - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1050 MPa
OENORM EN 4628-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm - 1150 MPa ≤ Rm ≤ 1300 MPa
OENORM EN 4627-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 1150 MPa ≤ Rm ≤ 1300 MPa
OENORM EN 4630-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1050 MPa
OENORM EN 2213-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bars - De <= 16 mm - 980 MPa <= Rm <= 1180 MPa
OENORM EN 3526-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm <= a <= 6 mm - 980 MPa <= Rm <= 1180 MPa
OENORM EN 3525-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Plates - 6 mm <= a <= 20 mm - 1080 MPa <= Rm <= 1280 MPa
OENORM EN 3523-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bar for machining - De <= 100 mm - 1080 MPa <= Rm <= 1280 MPa
OENORM EN 4825-2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1100 MPa
OENORM EN 3361-2021 Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Sheets and strips - a <= 6mm - 1070 MPa <= Rm <= 1220 MPa
OENORM EN 4884-2021 Aerospace series - Steel X3CrNiMoAl (13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - 1200 MPa ≤ Rm ≤ 1350 MPa

European Committee for Standardization (CEN), mp and mpa

prEN 4628-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ≤ 200 mm - 1150 MPa ≤ Rm ≤ 1300 MPa
prEN 4631-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bars - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1050 MPa
prEN 4627-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 1150 MPa ≤ Rm ≤ 1300 MPa
prEN 4630-2021 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 900 MPa ≤ Rm ≤ 1050 MPa
prEN 2213-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bars - De ≤ 16 mm - 980 MPa ≤ Rm ≤ 1180 MPa
EN ISO 14529-2:1999 Plastics - Melamine/Phenolic Powder Moulding Compounds (MP-PMCs) - Part 2: Preparation of Test Specimens and Determination of Properties ISO 14529-2:1999
EN 4720:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De ��200 mm - 1 150 MPa ��Rm ��1 300 MPa
prEN 3526-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm ≤ a ≤ 6 mm - 980 MPa ≤ Rm ≤ 1180 MPa
prEN 3524-2021 Aerospace series - Steel 15CrMoV6 (334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm ≤ a ≤ 6 mm - 1080 MPa ≤ Rm ≤ 1280 MPa
EN 4098:2007 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Remelted, hardened and tempered, forgings De less than or equal to 50 mm, 1 250 MPa less than or equal to Rm less than or equal to 1 400 MPa
prEN 3525-2021 Aerospace series - Steel 15CrMoV6 (334) - Air melted - Hardened and tempered - Plates - 6 mm ≤ a ≤ 20 mm - 1080 MPa ≤ Rm ≤ 1280 MPa
EN 4627:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ��200 mm - 1 150 MPa ��Rm ��1 300 MPa
EN 4630:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ��200 mm - 900 MPa ��Rm ��1 050 MPa
prEN 3523-2021 Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bar for machining - De ≤ 100 mm - 1080 MPa ≤ Rm ≤ 1280 MPa
EN 4721:2014 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted and electroslag remelted (ESR) - Hardened and tempered - Bar - De <= 200 mm - 900 MPa <= Rm<= 1050 MPa
EN 2540:2018 Aerospace series - Steel X7CrNiAl17-7 (1.4568) - Air melted - Solution treated and precipitation hardened - Sheet and strip - a ��6 mm - 1 240 MPa ��Rm ��1 450 MPa
EN 4825:2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1100 MPa
EN 4631:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ��200 mm - 900 MPa ��Rm ��1 050 MPa
EN 4627:2007 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Forgings - De less than or equal to 150 mm - 1 100 MPa less than or equal to Rm less than or equal to 1 300 MPa
EN 4628:2007 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Bar - De less than or equal to 150 mm - 1 100 MPa less than or equal to Rm less than or equal to 1 300 MPa
EN 4628:2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ��200 mm - 1 150 MPa ��Rm ��1 300 MPa
prEN 3361-2021 Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Sheets and strips - a ≤ 6 mm - 1070 MPa ≤ Rm ≤ 1220 MPa
prEN 3479-2021 Aerospace series - Steel X5CrNiCu155 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a ≤ 20 mm - 1070 MPa ≤ Rm ≤ 1220 MPa
EN 3361:2007 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a less than or equal to 6mm, 1 070 MPa less than or equal to Rm less than or equal to 1 220 MPa
EN 3120:2012 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ��D ��51 mm - 690 MPa ��Rm ��1 030 MPa
prEN 4884-2021 Aerospace series - Steel X3CrNiMoAl (13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars for machining - a or D ≤ 200 mm - 1200 MPa ≤ Rm ≤ 1350 MPa

European Association of Aerospace Industries, mp and mpa

AECMA PREN 2863-1993 Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/315 Degrees C Edition P 1; Corrigendum 05/10/1993
AECMA PREN 2865-1989 Aerospace Series Nuts, Anchor, Self-Locking, Two Lug, Floating, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1100 MPa (at Ambient Temperature)/315 Degrees C Edition 1
AECMA PREN 2865-1993 Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/315 Degrees C Edition P 1
AECMA PREN 2866-1992 Aerospace Series Nuts, Anchor, Self-Locking, Floating, One Lug, with Counterbore, in Steel, Cadmium Plated, MoS2 Lubricated Classification : 1 110 MPa (at Ambient Temperature) / 235 Degrees C Issue P 1
AECMA PREN 2867-1992 Aerospace Series Nuts, Anchor, Self-Locking, Floating, One Lug, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 110 MPa (at Ambient Temperature) / 315 Degrees C Issue P 1
AECMA PREN 2868-1993 Aerospace Series Nuts, Hexagonal, Slotted/Castellated, Normal Height, Normal Across Flats, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 650 Degrees C Edition P 1
AECMA PREN 2869-1991 Aerospace Series Nuts, Hexagonal, Slotted/Castellated, Normal Height, Normal Across Flats, in Heat Resisting Steel, Passivated Classification : 1100 MPa (at Ambient Temperature) / 650 Degrees Celsius Edition 1
AECMA PREN 3513-1988 Aerospace Series Steel FE-PL711 Hardened and Tempered 900 Less Than or Equal to Rm Less Than or Equal to 1100 MPa Bar and Wire De Less Than or Equal to 45 mm Issue P 1
AECMA PREN 3514-1988 Aerospace Series Steel FE-PL711 Hardened and Tempered 1100 Less Than or Equal to Rm Less Than or Equal to 1300 MPa Bar and Wire for Bolts De Less Than or Equal to 25 mm Issue P 1

Lithuanian Standards Office , mp and mpa

LST EN ISO 14529-1:2001 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 1: Designation system and basis for specifications (ISO 14529-1:1999)
LST EN ISO 14529-2:2001 Plastics - Melamine/phenolic powder moulding compounds (MP-PMCs) - Part 2: Preparation of test specimens and determination of properties (ISO 14529-2:1999)
LST EN 4628-2013 Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ? 200 mm - 1 150 MPa ? Rm ? 1 300 MPa
LST EN 4825-2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ? 150 mm - 900 MPa ? Rm ? 1 100 MPa
LST EN 3639-2021 Aerospace series - Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) - Softened and cold worked - Wires for forged fasteners - D ? 15 mm - 900 MPa ? Rm ? 1 100 MPa

Aerospace Industries Association/ANSI Aerospace Standards, mp and mpa

AIA/NAS NA0271-2014 PROCUREMENT SPECIFICATION, METRIC FASTENERS, CRES 300 SERIES, EXTERNALLY THREADED, MJ THREAD, 500 MPa Ftu and 700 MPa Ftu (Rev 2)

AIA/NAS - Aerospace Industries Association of America Inc., mp and mpa

NA0271-2014 PROCUREMENT SPECIFICATION@ METRIC FASTENERS@ CRES 300 SERIES@ EXTERNALLY THREADED@ MJ THREAD@ 500 MPa Ftu and 700 MPa Ftu (Rev 2)
NA0271-2011 PROCUREMENT SPECIFICATION@ METRIC FASTENERS@ CRES 300 SERIES@ EXTERNALLY THREADED@ MJ THREAD@ 500 MPa Ftu and 700 MPa Ftu (Rev 1)
NA0033-0034-2014 NUT@ SELF-LOCKING@ HEXAGON@ EXTENDED WASHER 1100 MPa@ METRIC@ 235 °C AND 425 °C (Rev 4)
NA0096-2018 NUT@ SELF-LOCKING@ PLATE@ CORNER@ CRES@ LOW HEIGHT@ CBORE@ 900 MPa@ METRIC@ 235 °C AND 425 °C (Rev 4)
NA0096-2012 NUT@ SELF-LOCKING@ PLATE@ CORNER@ CRES@ LOW HEIGHT@ CBORE@ 900 MPa@ METRIC@ 235 °C AND 425 °C (Rev 3)

Professional Standard - Chemical Industry, mp and mpa

HG/T 5135~5138-2016 Fluorescent whitening agent MP (fluorescent whitening agent ER-Ⅴ), fluorescent whitening agent OB-2, CI reaction yellow 174 and CI reaction blue 72 (2016)

CH-SNV, mp and mpa

SN EN 4825-2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1100 MPa

American Society for Testing and Materials (ASTM), mp and mpa

ASTM D8322-20 Standard Test Method for Determination of Elements in Residual Fuels and Crude Oils by Microwave Plasma Atomic Emission Spectroscopy (MP-AES)
ASTM F3125/F3125M-22 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 M
ASTM F3125/F3125M-18 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 MPa and 1040 MPa Minimum Tensile Strength
ASTM F3125-15 Standard Specification for High Strength Structural Bolts, Steel and Alloy Steel, Heat Treated, 120 ksi (830 MPa) and 150 ksi (1040 MPa) Minimum Tensile Strength, Inch and Metric Dimensions
ASTM F3125/F3125M-15a Standard Specification for High Strength Structural Bolts, Steel and Alloy Steel, Heat Treated, 120 ksi (830 MPa) and 150 ksi (1040 MPa) Minimum Tensile Strength, Inch and Metric Dimensions
ASTM D8351-22 Standard Test Method for Determination of Trace Elements in Biodiesel and Biodiesel Blends by Microwave Plasma Atomic Emission Spectrometry (MP-AES)
ASTM F3125/F3125M-21 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 M
ASTM F3125/F3125M-19 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 M
ASTM F3125/F3125M-19e1 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 M
ASTM F3125/F3125M-19e2 Standard Specification for High Strength Structural Bolts and Assemblies, Steel and Alloy Steel, Heat Treated, Inch Dimensions 120 ksi and 150 ksi Minimum Tensile Strength, and Metric Dimensions 830 M

IT-UNI, mp and mpa

UNI EN 4825-2021 Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De 150 mm - 900 MPa Rm 1 100 MPa
UNI EN 3639-2021 Aerospace series - Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) - Softened and cold worked - Wires for forged fasteners - D ≤ 15 mm - 900 MPa ≤ Rm ≤ 1 100 MPa

European Telecommunications Standards Institute (ETSI), mp and mpa

ETSI TR 101 904-2001 Transmission and Multiplexing (TM); Time Division Duplex (TDD) in Point-To-Multipoint (P-MP) Fixed Wireless Access (FWA) Systems; Characteristics and Network Applications

ETSI - European Telecommunications Standards Institute, mp and mpa

TR 101 904-2001 Transmission and Multiplexing (TM); Time Division Duplex (TDD) in Point-To-Multipoint (P-MP) Fixed Wireless Access (FWA) Systems; Characteristics and Network Applications (V1.1.1)
ETSI EN 300 631-2:1999 Transmission and Multiplexing (TM); Digital Radio Relay Systems (DRRS); Part 2: Antennas for Point-to-Multipoint (P-MP) Radio Links in the 1 GHz to 3 GHz Band (V1.1.1)

KR-KS, mp and mpa

KS W ISO 8538-2020 Aerospace — Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 °C, 1 100 MPa (at ambient temperature)/315 °C a
KS W ISO 9156-2020 Aerospace — Nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, with MJ threads, classifications:1 100 MPa (at ambient temperature)/235 °C,1 100 MPa (at ambient temperatur

PL-PKN, mp and mpa

PN-EN 4825-2021-10 E Aerospace series -- Steel X12CrNiMoV12-3 (1.4938) -- Air melted and consumable electrode remelted -- Hardened and tempered -- Bars -- De ≤ 150 mm -- 900 MPa ≤ Rm ≤ 1 100 MPa
PN H74739-1988 Valves and pipelines Loose flanges for flanged tubes for pressure class 0,25-i-1,6 MPa

未注明发布机构, mp and mpa

DIN EN 3761:1994 Aerospace series — Heat resisting alloy FE-PA2601 — Softened and cold worked — Bar for forged fasteners D<50 mm, 1 100 MPa
BS 2S 510:1970(2003) Specification for carbon steel sheet and strip (430 / 540 MPa) (suitable for welding)
BS 2S 143:1976(2001) Specification for Chromium - nickel - copper - molybdenum corrosion - resisting steel (precipitation hardening) billets, forgings and parts (93 & 1080 MPa)
BS 5S 82:1976(2003) Specification for 4 % nickel - chromium - molybdenum case - hardening steel billets, bars, forgings and parts (1320 – 1520 MPa)

CZ-CSN, mp and mpa

CSN 63 5314 Z2-1998
CSN 13 9703-1975 Machined ends of pipes and fittings for working excess pressure 32 MPa (≌ 325 kp/cm2)
CSN 13 9731-1975 Precision and elastic precision screw studs for working excess pressure 32 MPa (≌ 325kp/om2)
CSN 10 9400-1982 United system of industrial pneumatic components. Non-return valves, pn 0,63 and 1,0 MPa Series of size

GM North America, mp and mpa

GM GMP.EEBC.003-2001 Thermoplastic Polyester Elastomer - 73 Type D Hardness, 560 MPa Flexural Modulus
GM GMP.EEBC.004-2001 Thermoplastic Polyester Elastomer - 47 Type D Hardness, 90 MPa Flexural Modulus
GM GMP.EEBC.007-2002 Thermoplastic Polyester Elastomer - 62 Type D Hardness, 300 MPa Flexural Modulus
GM GMP.EEBC.008-2001 Thermoplastic Polyester Elastomer - 55 Type D Hardness, 200 MPa Flexural Modulus
GM GMP.EEBC.012-2002 Thermoplastic Polyester Elastomer - 49 Type D Hardness, 195 MPa Flexural Modulus
GM GMP.EEBC.013-2002 Thermoplastic Polyester Elastomer - 49 Type D Hardness, 87 MPa Flexural Modulus
GM GMP.EEBC.014-2001 Thermoplastic Polyester Elastomer - 55 Type D Hardness, 520 MPa Flexural Modulus
GM GMP.EEBC.015-2001 Thermoplastic Polyester Elastomer - 55 Type D Hardness, 400 MPa Flexural Modulus

RU-GOST R, mp and mpa

GOST R 55600-2013 Pipes and pipeline components for pressure over 100 to 320 MPa. Norms and methods of strength calculation
GOST R 55599-2013 High pressure pipeline assembly units and components above 10 up to 100 MPa. General technical requirements
GOST 9789-1975 Safety full-lifted flanged steel valve for Pnom 1,6 and 4,0 MPa (16 and 40 kgf/sq sm). Specifications
GOST 19500-1974 Malleable iron chaklift screwed and flanged valves for pnom 1,6 mpa (16 kgf/sg cm)

CEN - European Committee for Standardization, mp and mpa

EN 3470:2019 Aerospace series - Steel FE-PM1503 (X3CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - 1 200 MPa ≤ Rm ≤ 1 400 MPa