RM
RM, Total:147 items.
The international standard classification for "RM" includes: Magnetic components .
The Chinese standard classification for "RM" includes: Industrial electric heating equipment , Inductor and transformer , Magnetic component .
Professional Standard - Machinery
- JB/T 8195.2-1999 Indirect resistance furnaces RM series box-type quenching furnaces
Professional Standard - Electron
- SJ 51931/7-1998 Detail specification for R7K soft-ferrite RM Type serial cores
- SJ/T 2744-2002 Dimensions of spuare cores (RM cores) made of magnetic oxides and associated parts
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
- GB/T 9634.2-2002 Ferrite cores0--Guide on limits of surface irregularities--Part 2:RM-cores
Group Standards of the People's Republic of China
- T/CNTAC RM1-2019 Cotton rubbing cloth of rubbing tests for textiles colour fastness
Taiwan Provincial Standard of the People's Republic of China
- CNS 14648-2002 Management of the transport network-Application of the RM-ODP framework
International Organization for Standardization (ISO)
- ISO/TR 10989:2009 Reference materials - Guidance on, and keywords used for, RM categorization
- ISO 19153:2014 Geospatial Digital Rights Management Reference Model (GeoDRM RM)
RU-GOST R
- GOST 15819-1985 Oils RM and RMC. Specifications
Spanish Association for Standardization (UNE)
- UNE-EN 4685:2011 Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm >= 1 240 MPa (Endorsed by AENOR in August of 2011.)
- UNE-EN 3460:2019 Aerospace series - Titanium TI-P99002 - Annealed - Bar for machining - a or D = 150 mm - Rm = 390 MPa
- UNE-EN IEC 63093-4:2019 Ferrite cores - Guidelines on dimensions and the limits of surface irregularities - Part 4: RM-cores (Endorsed by Asociación Española de Normalización in June of 2019.)
- UNE-ISO/TR 10989:2014 IN Reference materials - guidance on, and keywords of, RM categorization
- UNE-EN 2399:2008 Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm >= 900 MPa - Bars for forged bolts - D <= 25 mm (Endorsed by AENOR in June of 2008.)
- UNE-EN 2398:2008 Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm >= 900 MPa - Bars for machined bolts - D <= 25 mm (Endorsed by AENOR in May of 2008.)
- UNE-EN 3161:2007 Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D <= 200 mm, Rm >= 930 MPa (Endorsed by AENOR in November of 2007.)
- UNE-EN 4318:2007 Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De <= 100 mm, Rm >= 960 MPa (Endorsed by AENOR in November of 2007.)
- UNE-EN 3678:2007 Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted - Solution treated and precipitation treated - Forgings - a or D =< 200 mm - Rm =>930 MPa (Endorsed by AENOR in May of 2007.)
British Standards Institution (BSI)
- BS EN 2502:2019 Aerospace series. Steel X5CrNoMoCuNb14-5 (1.4594). 930 MPa ≤ Rm ≤ 1 080 MPa. Bars
- BS EN 60424-2:2016 Ferrite cores. Guidelines on the limits of surface irregularities. RM-cores
- BS EN 2450:2018(2019) Aerospace series — Steel 31Ni10 — 1230 MPa ≤ Rm ≤ 1420 MPa — Bars — De ≤ 40 mm
- BS EN 2461:2009 Aerospace series - Steel FE-PM1901 (X12CrNi13) - 600 MPa
Rm 800 MPa - Forgings - De 70 mm - BS EN 4675:2011(2015) Aerospace series — Titanium Ti - P63002 (Ti5Al5Mo5V3Cr0.4Fe) — Rm > 1300 MPa — Bars — De < 110 mm
- BS EN 62317-4:2005(2018) Ferrite cores - Dimensions Part 4 : RM - cores and associated parts
- BS EN 2478:2008 Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1220 MPa
Rm 1370 MPa - Bars - De 40 mm - BS EN 2446:2008 Aerospace series - Steel FE-PL1503 (35CrMo4) - 1100 MPa
Rm 1300 MPa - Bars - De 25 mm - BS EN 2481:2010(2011) Aerospace series — Steel FE - PL2108 (36NiCrMo16) — 1250 MPa Rm 1400 MPa — Forgings — De 75 mm
- BS EN 2483:2010(2011) Aerospace series — Steel FE - PL2108 (36NiCrMo16) — 1100 MPa Rm 1300 MPa — Forgings — De 100 mm
- BS EN 2438:2008 Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa
Rm 1100 MPa - Bars - De 40 mm - BS EN 2439:2009 Aerospace series - Steel FE-PL2102 (34NiCr6) - 900 MPa
Rm 1100 MPa - Forgings - De 40 mm - BS EN IEC 63093-4:2019 Ferrite cores. Guidelines on dimensions and the limits of surface irregularities - RM-cores
- BS EN 2448:2008 Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa
Rm 1100 MPa - Bars - De 40 mm - BS EN 2482:2010(2011) Aerospace series — Steel FE - PL2108 (36NiCrMo16) — 1100 MPa Rm 1300 MPa — Bars — De 100 mm
- BS EN 2460:2009 Aerospace series - Steel FE-PM1901 (X12CrNi13) - 600 MPa
Rm 800 MPa - Bars - De 70 mm - BS EN 2206:2008 Aerospace series - Steel FE-PL1502 (25CrMo4) - 650 MPa
Rm 850 MPa - Bars - De 150 mm - BS EN 2480:2008 Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1250 MPa
Rm 1400 MPa - Bars - De 75 mm - BS EN 2278:2014 Aerospace series. Steel X12CrNiMoV12-3 (1.4933). 900 MPa
Rm 1 100 MPa. Bars. De 150 mm - BS EN 2205:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa
Rm 1100 MPa - Bars - De 40 mm - BS EN 2451:2019 Aerospace series. Steel 31Ni10. 1 230 MPa ≤ Rm ≤ 1 420 MPa. Forgings. De ≤ 40 mm
- BS EN 4904:2022 Aerospace series. Steel 36NiCrMo16 (1.6773). 1 000 MPa ≤ Rm ≤ 1 200 MPa. Bars. 100 mm ≤ D ≤ 250 mm
- BS EN 2137:2017 Aerospace series. Steel FE-PL75. 1 100 MPa ≤ Rm ≤ 1 250 MPa. Bars. De ≤ 100 mm
- BS EN 2503:2019 Aerospace series. Steel X5CrNoMoCuNb14-5 (1.4594). 930 MPa ≤ Rm ≤ 1 080 MPa. Forgings. De ≤ 150 mm
- BS EN 2476:2019 Aerospace series. Steel 30CrNiMo8 (1.6580). 1 100 MPa ≤ Rm ≤ 1 300 MPa. Forgings. De ≤ 100 mm
- BS EN 2252:2012 Aerospace series. Steel FE-PL1505 (15CrMoV6). 1080 MPa
Rm 1250 MPa. Forgings. De 100 mm - BS EN 2573:2007 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Softened - Rm
780 MPa - Wire - 0,25 mm De 3 mm - BS EN 2279:2018 Aerospace series. Steel FE-PM37. 900 MPa
Rm 1 100 MPa. Forgings. De 150 mm - BS ISO 19153:2014 Geospatial Digital Rights Management Reference Model (GeoDRM RM)
- BS EN 2399:2008(2011) Aerospace series — Heat resisting steel FE - PA2601 (X4NiCrTiMoV26 - 15) — Rm 900 MPa — Bars for forged bolts — D 25 mm
- BS EN 2398:2008(2013) Aerospace series — Heat resisting steel FE - PA2601 (X6NiCrTiMoV26 - 15) — Rm ≥ 900 MPa — Bars for machined bolts — D ≤ 25 mm
- BS EN 2280:2018 Aerospace series. Steel FE-PM37. 900 MPa
Rm 1 100 MPa. Sheet. a 6 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 EN 3460:2019 Aerospace series. Titanium TI-P99002. Annealed. Bar for machining. a or D ≤ 150 mm. Rm ≥ 390 MPa
- BS EN 4528:2009 Aerospace series - Steel FE-PA 3903 (X10CrNi18-8) - Cold rolled - Strip for springs - a
3 mm - 1250 MPa Rm 1640 MPa - BS EN 3468:2019 Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 MPa ≤ Rm ≤ 700 MPa. Forgings. De ≤ 100 mm
- BS EN 3489:2019 Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 ≤ Rm ≤ 750 MPa. Tubes for structures. 0,5 ≤ a ≤ 5 mm
- BS 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
- BS EN 4263:2013 Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D
200 mm - 690 MPa Rm 960MPa - BS EN 4098:2007 Aerospace series - Steel FE-PL1507 (40CrMoV12) - Remelted, hardened and tempered, forgings De
50 mm, 1250 MPa Rm 1400 MPa - BS EN 2469:2007 Aerospace series - Steel FE-PA3901 (X1CrNi18-10) - Air melted - Softened - Wires - 0,4 mm
D 12,5 mm - 450 MPa Rm 650 MPa - BS EN 2302:2023 Aerospace series. Heat-resisting nickel base alloy NiCr20Co3Fe3. Rm ≥ 650 MPa. Sheets and strips, cold rolled. 0,25 mm < a ≤ 3 mm
- 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 3355:2012(2017) Aerospace series — Titanium alloy TI - P64001 (Ti - 6Al - 4V) — Annealed — Extruded section — De ≤ 150 mm — 900 MPa ≤ Rm ≤ 1160 MPa
- BS EN 4262:2013 Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D
200 mm - 690 MPa Rm 880MPa - BS EN 3488:2024 Aerospace series. Steel X6CrNiTi18-10 (1.4541). Air melted. Softened. Sheets and strips. a ≤ 6 mm. 500 MPa ≤ Rm ≤ 700 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 EN 4631:2024 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 2213:2012 Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bars. De
16 mm. 980 MPa Rm 1180 MPa - BS EN 3525:2023 Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Plates. 6 mm ≤ a ≤ 20 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa
- BS 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 1050 MPa - BS EN 2174:2017(2018) Aerospace series - Heat resisting alloy FE - PA2602 (X4NiCrTiMoV26 - 15) - Solution treated and precipitation treated - Forgings - De ≤ 100 mm - Rm ≥ 850 MPa
- BS EN 3507:2006 Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Forgings - De ≤100 mm - 930 MPa ≤ Rm ≤ 1 080 MPa
- BS EN 3491:2006 Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Forgings - De u 100 mm - 900 MPa u Rm u 1 100 MPa
- BS EN 4630:2024 Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Forgings. De ≤ 200 mm. 900 MPa ≤ Rm ≤ 1 050 MPa
- BS EN 3488:2007 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Sheet and strip - a
6 mm - 500 MPa Rm 700 MPa - BS EN 3486:2019 Aerospace series. Steel X3CrNiMoAl13-8-2 (1.4534). Solution annealed and precipitation hardened. 1 400 ≤ Rm ≤ 1 550 MPa. Forgings. De ≤ 100 mm
- BS EN 4627:2007 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Forgings - De
150 mm - 1100 MPa Rm 1300 MPa
German Institute for Standardization
- DIN EN 2480:2009 Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa
R<(Index)m> 1400 MPa - Bars - D<(Index)e> 75 mm; German and English version EN 2480:2008 - DIN EN 2206:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 650 MPa
R<(Index)m> 850 MPa - Bars - D<(Index)e> 150 mm; German and English version EN 2206:2008 - DIN EN 2137:2017 Aerospace series - Steel FE-PL75 - 1100 MPa <= Rm <= 1250 MPa - Bars - De <= 100 mm; German and English version FprEN 2137:2017
- DIN EN 2279:2018 Aerospace series - Steel FE-PM37 - 900 MPa <= Rm <= 1100 MPa - Forgings - De <= 150 mm; German and English version EN 2279:2018
- DIN EN 2478:2009 Aerospace series - Steel FE-PL2107 (30NiCrMo16) - 1220 MPa
R<(Index)m> 1370 MPa - Bars - D<(Index)e> 40 mm; German and English version EN 2478:2008 - DIN EN 2280:2018 Aerospace series - Steel FE-PM37 - 900 MPa <= Rm <= 1 100 MPa - Sheet - a <= 6 mm; German and English version EN 2280:2018
- DIN EN 2279 E:2017-12 Aerospace series - Steel FE-PM37 - 900 MPa <= Rm <= 1100 MPa - Forgings - De <= 150 mm
- DIN EN 2280 E:2017-12 Aerospace series - Steel FE-PM37 - 900 MPa <= Rm <= 1 100 MPa - Sheet - a <= 6 mm
- DIN EN 60424-2 E:2013-05 Ferrite cores - Guidelines on the limits of surface irregularities - Part 2: RM-cores
- DIN EN 2278 E:2014-07 Aerospace series - Steel X12CrNiMoV12-3 (1.4933) - 900 MPa <= Rm <= 1100 MPa, Bars - De <= 150 mm
- DIN EN 62317-4:2006 Ferrite cores - Dimensions - Part 4: RM-cores and associated parts (IEC 62317-4:2005); German version EN 62317-4:2005
- DIN EN 60424-2:1998 Guidance on the limits of surface irregularities of ferrite cores - Part 2: RM-cores (IEC 60424-2:1997); German version EN 60424-2:1997
- DIN EN IEC 63093-4:2019-11 Ferrite cores - Guidelines on dimensions and the limits of surface irregularities - Part 4: RM-cores (IEC 63093-4:2019); German version EN IEC 63093-4:2019 / Note: DIN EN 60424-2 (2016-10), DIN EN 62317-4 (2006-07) and DIN EN 62317-4 Berichtigung 1 (20...
- DIN EN 2278 E:1980-11 Aerospace series - Steel X12CrNiMoV12-3 (1.4933) - 900 MPa <= Rm <= 1100 MPa, Bars - De <= 150 mm
- DIN EN 2398:2009 Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - R<(Index)m>
900 MPa - Bars for machined bolts - D 25 mm; German and English version EN 2398:2008 - DIN EN 2465:2008 Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Softened - 450 MPa
R<(Index)m> 680 MPa - Bar for machining - 4 mm D<(Index)e> 100 mm; German and English version EN 2465:2007 - DIN EN 2399:2009 Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - R<(Index)m>
900 MPa - Bars for forged bolts - D 25 mm; German and English version EN 2399:2008 - DIN EN 2209:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa
R<(Index)m> 1100 MPa - Sheets, strips and plates - 0,5 mm a 20 mm; German and English version EN 2209:2008 - DIN EN 2465 E:2019-04 Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Softened - 450 MPa
R<(Index)m> 680 MPa - Bar for machining - 4 mm D<(Index)e> 100 mm - DIN EN 3480:2008 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Plate - 6 mm
a 50 mm - 500 MPa R<(Index)m> 700 MPa; German and English version EN 3480:2007 - DIN EN 2461:2009 Aerospace series - Steel FE-PM1901 (X12CrNi13) - 600 MPa
R<(Index)m> 800 MPa - Forgings - D<(Index)e> 70 mm; German and English version EN 2461:2009 - DIN EN 2439:2009 Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa
R<(Index)m> 1100 MPa - Forgings - D<(Index)e> 40 mm; German and English version EN 2439:2009 - 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 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 2174:2017 Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Forgings - De <= 100 mm - Rm >= 850 MPa; German and English version FprEN 2174:2017
- DIN EN 3480 E:2022-03 Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Plate - 6 mm
a 50 mm - 500 MPa R<(Index)m> 700 MPa - 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 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 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 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 EN 4627 E:2014-02 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
- DIN EN 2467:2008 Aerospace series - Steel FE-PA3901 (X2CrNi18-9) - Air melted - Softened - Plate, sheet and strip - 0,4 mm
a 20 mm - 520 MPa R<(Index)m> 670 MPa; German and English version EN 2467:2007
International Electrotechnical Commission (IEC)
- IEC 60424-2:2015 Ferrite cores - Guidelines on the limits of surface irregularities - Part 2: RM-cores
- IEC 62317-4:2005 Ferrite cores - Dimensions - Part 4: RM-cores made of ferrite and associated parts
- IEC 62317-4:2005/COR1:2016 Corrigendum 1 - Ferrite cores - Dimensions - Part 4: RM-cores and associated parts
- IEC 63093-4:2019 Ferrite cores - Guidelines on dimensions and the limits of surface irregularities - Part 4: RM-cores
European Association of Aerospace Industries
- AECMA PREN 2171-1979 Heat Resisting Steel FE-PA92-HT Rm Greater Than or Equal to 900 MPa Bars Aerospace Series Edition 1
Australian/New Zealand Standard (AU-AS/NZS)
- AS/NZS ISO 19153:2015 Geospatial Digital Rights Management Reference Model (GeoDRM RM)
International Dairy Federation (IDF)
- IDF/RM 150-2012 Fremented milks - Determination of titratable acidity - Potentiometric method
- IDF/RM 215-2006 Milk and milk products. Determination of antimicrobial residues.Tube diffusion test
- IDF/RM 225-2009 Milk and milk products - Method for the enumeration of Pseudomonas spp.
European Committee for Standardization (CEN)
- EN 2446:2008 Aerospace series - Steel FE-PL1503 (35CrMo4) - 1 100 MPa less than or equal to Rm less than or equal to 1 300 MPa - Bars - De less than or equal to 25 mm
- prEN 2274-1979 Aerospace series; steel FE-PA 95; 1750 MPa
<(kursiv)R><(Index)m> 2000 MPa; bars <(kursiv)D><(Index)e> 150 mm - prEN 2313-1981 Steel FE-PM42, R<(Index)m>
1350 MPa; bars D<(Index)e> 100 mm; aerospace series - prEN 2278-1981 Steel FE-PM37, 900 MPa
R<(Index)m> 1100 MPa; bars D<(Index)e> 150 mm; aerospace series - prEN 2280-1981 Steel FE-PM37, 900 MPa
R<(Index)m> 1100 MPa; sheet a 6 mm; aerospace series - prEN 2214-1981 Steel FE-PL52 S, 1080 MPa
R<(Index)m> 1250 MPa; bars D<(Index)e> 100 mm; aerospace series - prEN 2228-1977 Aerospace series; steel FE-PA 12; 500 MPa
<(kursiv)R><(Index)m> 700 MPa; sheets 0,5 mm <(kursiv)a> 6 mm - prEN 2206-1981 Steel FE-PL43 S, 650 MPa
R<(Index)m> 850 MPa; bars D<(Index)e> 150 mm; aerospace series - prEN 2213-1981 Steel FE-PL52 S, 980 MPa
R<(Index)m> 1180 MPa; bars D<(Index)e> 16 mm; aerospace series - prEN 2136-1981 Aerospace series; steel FE-PM 42; 900 MPa
R<(Index)m> 1100 MPa; bars D<(Index)e> 100 mm - prEN 2205-1981 Steel FE-PL43 S, 900 MPa
R<(Index)m> 1100 MPa; bars D<(Index)e> 40 mm; aerospace series - prEN 2171-1981 Heat resisting steel FE-PA92-HT, R<(Index)m>
900 MPa; bars; aerospace series - prEN 2216-1981 Steel FE-PL52 S, 1050 MPa
R<(Index)m> 1250 MPa; sheets a 2 mm; aerospace series
PH-BPS
- PNS ISO/TR 10989:2021 Reference materials - Guidance on, and keywords used for, RM categorization
KR-KS
- KS A ISO TR 10989-2018(2023) Reference materials — Guidance on, and keywords used for, RM categorization
- KS A ISO TR 10989-2018 Reference materials — Guidance on, and keywords used for, RM categorization
YU-JUS
- JUS N.R8.052-1981 Magnetic materiah and components. RM-cores. General requirements.
- JUS N.R8.052-1979 Magnetic materiak and components. RM-cores. General requirements.
Association Francaise de Normalisation
- FD X07-030*FD ISO/TR 10989:2009 Reference materials - Guidance on, and keywords used for, RM categorisation
- NF L10-548:2008 Aerospace series - Steel FE-PM 3504 (X4CrNiMo16-5-1) - Air melted - Hardened and tempered - Bar - De < or = 200 mm - 900 MPa < or = Rm < or = 1 050 MPa.
- NF Z52-047:2014 Geospatial digital rights management reference model (GeoDRM RM)
RO-ASRO
- STAS 10918-1977 Fcromagnetic oxide materials.FERRITE SQUARE CORES (RM) Dimensions
ASD-STAN - Aerospace and Defence Industries Association of Europe - Standardization
- PREN 3312-1988 Titanium Alloy TI-P63 Annealed 900 Less Than or Equal to Rm Less Than or Equal to 1160 MPa Forgings De Less Than or Equal to 150 mm
SCC
- ASD-STAN prEN 2776:1970 Steel FE-P11 - Rm <or= 340 MPa - Sheet and strip - a <or= 2 mm
- DANSK DS/ISO 19153:2014 Geospatial Digital Rights Management Reference Model (GeoDRM RM)
PL-PKN
- PN H93460 ArkusZ05-1973 Standart ?uality carbon steel une?ual angles with Rm under 50 kG/mm2
Korean Agency for Technology and Standards (KATS)
- KS A ISO TR 10989:2018 Reference materials — Guidance on, and keywords used for, RM categorization
- KS A ISO TR 10989-2023 References Guidance and keywords for RM classification
Aerospace, Security and Defence Industries Association of Europe (ASD)
- ASD-STAN PREN 2172-2010 Aerospace series Heat resisting steel FE-PA92-HT Rm = 900 MPa Forgings Edition P2
Lithuanian Standards Office
- LST EN 4685-2011 Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm ? 1 240 MPa
RM,rm-200a,rm1220,rm-odp,idf/rm+87,idf/rm51,idf/rm,material rm,rm50,RM 100,material rm,rm-200,rm2016,rm.5,rm《5,rm2014,rm1050mpa,eight rm,rm208