105×617mmR
Amunisi > Armour-piercing fin-stabilized discarding sabot (APFSDS)

Ada berbagai cara untuk mengukur nilai penetrasi. NATO menggunakan kriteria bahwa 50% peluru harus menembus pelat), sedangkan standar Soviet/Rusia lebih tinggi yaitu 80% harus melewati pelat). Menurut otoritas seperti Paul Lakowski, perbedaan kinerja bisa mencapai 8%.
| Penamaan | Asal | Desainer & produser | Tahun | Panjang keseluruhan | Berat keseluruhan | Bahan penetrator/massa | Jenis & berat propelan | Tekanan ruang | Kecepatan moncong | Penurunan kecepatan | subproyektil tanpa sabot / dengan sabot | Perforasi pada kejadian normal dan miring | Catatan |
| --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- |
| M735 |  United States | Teledyne Firth Stirling | 1977 | 963 mm | 17.91 kg | Tungsten alloy X11 (core) / 2.16 kg with maraging steel jacket | 5.67 kg of M30 | 415 MPa | 1501 m/s | 67 m/s (at 1000 m) 133 m/s (at 2000nbsp;m) | 3.72 kg / 5.797 kg | NATO Heavy Single target at 2930 m (1307 m/s) | First serial production APFSDS of the United States.  Developed from the 152mm XM578E1 projectile, with increased core length and mass, as well as projectile body length.  XM735E2 Standardized as M735 around 1976. |
| M735A1 |  United States | Primex Technologies | 1979 | 963 mm |  | depleted uranium alloy (core) / 2.2 kg | 5.67 kg of M30 |  | 1501 m/s |  |  | ≈370 mm at 0° at 1000 m | A further modification of M735, using a depleted uranium core instead of the tungsten alloy core. Never fielded by the U.S. military. |
| M774 |  United States | Primex Technologies | 1980 | 908.05 mm | 17.146 kg | Depleted Uranium alloy / 3.4 kg | 5.89 kg of M30 |  | 1509 m/s | 67 m/s (at 1000 m) 134 m/s (at 2000 m) | 3.61 kg / 5.775 kg | 189 mm at 60° at 1000 m | First production monobloc penetrator used by US military tank fleets. |
| M833 |  United States | Primex Technologies | 1983 | 998.7 mm | 17.32 kg | Depleted uranium alloy / 3.665 kg | 5.8 kg of M30 |  | 1494 m/s | 54 m/s (at 1000 m) 107 m/s (at 2000 m) | / 6.192 kg | 420 mm LoS at 60° at 2000 m | Second production monobloc round for the 105mm M68 Gun produced by the US, had an increased length to diameter ratio. |
| M900A1 |  United States | Primex Technologies | 1991 | 1003 mm | 18.5 kg | Depleted uranium alloy / 3.83 kg or 4.246 kg | M43 LOVA |  | 1505 m/s |  | / 6.86 kg |  | Compared to the cancelled XM900 prototype, the M900A1 uses a new sabot, penetrator, and propellant. Designed for the M68A1 and M68A1E4 guns. |
| FP105 |  United States | Flinchbaugh Company & General Defense Corporation | 1980s | 927 mm | 18 kg | tungsten alloy | 6.1 kg of M30 or NQ-M044 | 410 MPa | 1485 m/s with NQ/M propellant 1510 m/s with M30 propellant |  | 3.6 kg / 5.8 kg | NATO Heavy Single target in excess of 4000 m and NATO Heavy triple target at 65° obliquity in excess of 6000 m | Similar design to the M774, also known as C-76 or C-76A1 in Canada |
| C127 |  United States/ Canada | Olin Ordnance Ammunition and SNC Industrial Technologies Inc | 1991 or 1992 |  |  | tungsten alloy | 6  kg of Olin cool-burnin BALL or M30 (optional) | 411 MPa | 1555 m/s-1560 m/s |  | 3.44 kg / 5.8 kg | 152 mm at 72° obliquity, 470 mm at 0° obliquity, both at range of 2000 m |  |
| CMC 105 |  United States | Chamberlain Manufacturing Corporation | early 1990s | 998.73 mm | 17.15 kg | tungsten alloy / 3.31 kg | 6.1 kg of M30 | 415 MPa | 1501 m/s | 55 m/s | 3.56 kg / 5.8 kg | NATO Heavy Single target at 4000 m and Heavy Triple at 5700 m or 178 mm at 67° obliquity at range about 2600 m | The latest private venture 105 mm APFSDS-T to be developed by the Chamberlain Manufacturing Corporation. |
| M111 Hetz-6 |  Israel | IMI | 1978 | 885 mm | 18.7 kg | tungsten alloy | 5.8 kg of M30 M | 420 MPa 436 MPa (max) | 1455 m/s | 48 m/s (at 1000 m) | 4.2 kg / 6.275 kg | NATO Heavy Single target at 2000 m or 150 mm at 60° obliquity at 2000 m or NATO Single Heavy at 4200 m | Produced under licence by Diehl in Germany and in Switzerland. Known as DM23 in the Bundeswehr, Pfeil Pat 78 Lsp in the Swiss Army and 33 mm Slpprj m/80 in the Swedish Army. Also produced by China, designated DTW1-105. |
| M413 Hetz-7 |  Israel | IMI | 1985 | 990 mm | 18.7 kg | tungsten alloy | 5.8 kg |  | 1450 m/s or 1455 m/s | 52 m/s (at 1000 m) | 4.1 kg / 6.3 kg | NATO Heavy Single target at 6000 m | Produced under licence by Diehl in Germany as DM33, also known as PPTFS M/85 LS in the Danish Army and under the CL260 designation on the export market. |
| M429 |  Israel | IMI | c. 1987 |  |  | tungsten alloy |  |  | 1450 m/s |  |  | Relatively equal performance to the M833 | Also known as FS Mk. 2 Improved in the South African Army or CL3108 (export designation) |
| M426  Hetz-10 |  Israel | IMI | 1990 | 990 mm | 19.2 kg | tungsten alloy | 6 kg of M26 | 440 MPa (nominal) | 1433 m/s or 1450 m/s |  | / 6.6 kg | 450 mm or 470 mm at 2000 m | Produced under licence by Diehl in Germany as DM63. Also known as FS Mk. 3 in the South African Army. Also used in modified versions by the Swedish Army (Slpprj m/90C and m/90S). |
| M428 SWORD |  Israel | IMI | 2003 | 1000 mm | 18.8 kg | tungsten alloy | 5.8 kg of NC-NG |  | 1505 m/s |  |  |  |  |
| 24 mm slpprj m/90C |  Israel/ Sweden | IMI | 1990 |  | 19.6 kg | tungsten alloy | 6 kg of NC-NG CEP 2 | 390 MPa | 1481 m/s |  | 4.4 kg / 6 kg |  | Modified version of the Israeli M426 APFSDS. |
| 24 mm slpprj m/90S |  Israel/ Sweden | IMI | 1990 |  | 19.6 kg | tungsten alloy | 6 kg of NC-NG CEP 2 | 460 MPa | 1560 m/s |  | 4.1 kg / 6 kg |  | Shortened variant (by 15.5 mm) of the Slpprj m/90C with a modified sabot to fit in the Strv 103 autoloader. |
| OFL 105 F1 |  France | GIAT | 1981 | 985 mm | 17.1 kg | 18 density tungsten alloy | 5.85 kg of B19T |  | 1495 m/s | 60 m/s (at 1000 m) | 3.8 kg / 5.8 kg | NATO Heavy Single target at 4400 m, NATO Heavy Triple target at 5000 m 392 mm at point-blank range, 370 mm at 1000 m, | Fitted with small bearing balls inside its hollow ballistic cap for improved beyond-armour effects against light armoured vehicles. |
| OFL 105 G2 |  France | GIAT | c. 1987 | 985 mm | 18 kg | tungsten-nickel-iron alloy | 5.85 kg of Wimmis |  | 1490 m/s | 138 m/s (at 2000 m) | 4.2 kg / 6.2 kg | NATO Heavy Single target at 6200 m, NATO Heavy Triple target at 7800 m 487 mm at point-blank range | The OFL 105 G2 uses a high energetic Swiss-made Wimmis double base propellant |
| OFL 105 G3 |  France | GIAT | c. 1987 | 985 mm |  | tungsten-nickel-iron alloy | 5.85 kg of B19T |  | 1460 m/s |  | 4.2 kg / 6.2 kg | NATO Heavy Single target at 5600 m, NATO Heavy Triple target at 7200 m 469 mm at point-blank range | cheaper variant (15%) of the OFL 105 G2 employing the standard SNPE poudre B propellant |
| OFL 105 F2 |  France | Giat Industries | 1995 | 990 mm | 18 kg | depleted uranium |  |  | 1525 m/s |  | / 6.25 kg | 520 mm or 540 mm at 2000 m | OFL 105 G2 variant with a DU penetrator |
| L64A4 |  United Kingdom | ROF Birtley | 1982 (L64A4) | 948 mm | 18.91 kg | tungsten alloy | 5.62 kg of WNC LM1900 | 426 MPa (nominal) 511 MPa (max) | 1480 m/s-1490 m/s |  | 3.59 kg / 6.12 kg | NATO Heavy Single target at 4200 m, NATO Heavy Triple target at 4800 m | 28 mm penetrator |
| H6/62 |  United Kingdom | ROF | 1987 | 990 mm | 18.5 kg | tungsten-nickel-iron alloy | 5.62 kg of WNC LM1900 | 426 MPa (nominal) 511 MPa (max) | 1490 m/s | 55 m/s (1000  m) | 3.59 kg / 6.12 kg | NATO Heavy Single target at 5000 m, NATO Heavy Triple targetat 6000 m, 360  mm at 2000 m | 25 mm penetrator |
| T-2-series |  United Kingdom | Royal Ordnance Speciality Metals | 1994 | 1030 mm | 19 kg | tungsten-nickel-iron alloy | multi-base granular |  | 1420 m/s | 48 m/s (1000  m) | 30 to 40% greater than that of current 105 mm APFSDS rounds | 540 mm RHA at 2000 m | Designed to be exclusively fired by the high pressure Royal Ordnance Improved Weapon System (IWS), the T-2-series APFSDS features a stub brass cartridge case and a combustible sleeve, penetrator diameter is 28 mm for a length-to-diameter ratio of 23:1. |
| DM43 |  Germany | Rheinmetall | late 1980s or early 1990s | 941 mm | 18 kg | tungsten alloy |  | 420 MPa | 1475 m/s |  | 4.3 kg / 6.1 kg or 6.3 kg | NATO triple heavy target at 5500 m |  |
| NP105A2 |  Austria | Ennstaler Metallwerk GmBH (designer) Noricum (producer) | 1984 | 980 mm | 19.3 kg | tungsten-nickel-iron, Tungalloy T-176FA alloy |  | 435 MPa (nominal) 495 MPa (max) | 1485 m/s | 72 m/s (1000  m) 128 m/s (2000  m) | 3.7 kg / | NATO Heavy Single Target at 5800 m, NATO Heavy Triple target at 6500 m and 473 mm at 1000 m or 127 mm of HD9 armour plate at 73° at unknown range. |  |
| HP 105 A2M |  Austria | Hirtenberger AG |  |  |  | T 176 tungsten alloy | 105-SCDB multitubular propellant | 430 MPa | 1535 m/s |  |  | NATO Heavy Single Target at more than 7000 m, NATO Heavy Triple target at 7500 m |  |
| C-437 |  Spain | Empresa Nacional Bazán and Santa Bárbara Sistemas | 1984 | 928 mm | 18 kg | tungsten alloy | 5.85 kg of B19T |  | 1485 m/s |  | / 5.65 kg | NATO Heavy Triple target and the Heavy Single target, both at 5000 m | Fitted with three DENAL wads under the windshield and around the penetrator core to prepare the penetration zone and prevents rebound from armour on impact at high angles of incidence. The penetration hole is between 60 and 70 mm in diameter. |
| C-512 |  Spain | Santa Bárbara Sistemas |  | 996 mm | 18 kg | tungsten alloy | 5.7 kg of B19T | 345 MPa | 1480 m/s |  | / 5.925 kg | NATO Heavy Triple target at 4550 m and 120 mm target at 70° at 3500 m | the C-512 is similar to the C-437 but use a slightly longer and heavier penetrator |
| NR 331 |  Belgium | PRB | 1980s |  |  | tungsten alloy |  |  |  |  |  |  |  |
| M1001 |  Belgium | MECAR | 1980s |  |  | tungsten alloy |  |  | 1525 m/s |  | 3.8 kg / 5.8 kg |  | is equivalent in performance to the FP105 APFSDS |
| M1050 |  Belgium | MECAR | late 1980s-early 1990s | 927 mm | 17.7 kg | tungsten alloy |  |  | 1510 m/s |  | / 5.8 kg |  | is equivalent in performance to the FP105 APFSDS |
| M1060A1 |  Belgium | MECAR | 1995 | 980 mm | 18 kg | tungsten-nickel-iron alloy |  |  | 1510 m/s |  | / 5.8 kg | 400 mm RHA at 60° LoS at 2000 m | Has comparable performance to the US M833 but without the problems associated with depleted uranium |
| M1060A2 |  Belgium | MECAR | late 1990s | 990 mm | 18.5 kg | tungsten alloy | 5.9 kg |  | 1450 m/s-1460 m/s |  | / 6.2 kg | 440 mm RHA at 60° LoS at 2000 m"105mm TK APFSDS-T M1060A2" (PDF). Nexter. 2018.  | This model of KE is a major product improvement of the MECAR M1060A1 APFSDS-T. |
| M1060A3 |  Belgium | MECAR | 2004 | 1000 mm | 18.7 kg | tungsten alloy | 6.2 kg of JA2 |  | 1560 m/s |  | / 6.2 kg | 500 mm RHA at 60° LoS at 2000 m |  |
| M1060CV |  Belgium | MECAR | 2004 |  |  | tungsten alloy | 6.2 kg of SCDB |  | 1620 m/s |  | / 6.2 kg | 560 mm RHA at 60° LoS at 2000 m | Designed for use with the Cockerill 105HP high-pressure gun. |
| XC127 Excalibur |  United States/ France/ United Kingdom | Primex Technologies, Giat Industries and RO Defence. | 1990s | 1010 mm |  | tungsten alloy X27X / 3.18 kg | 6 kg of BALL | 411 MPa (ball) to 414 MPa (granular) | 1560 m/s |  | / 5.8 kg | ≥480 mm RHA at 0° obliquity or 150 mm RHA at 72° both at 2000 m | Exhibits similar penetration performance to the first generation of 120 mm APFSDS rounds. |
| Type 93 |  Japan | Daikin | 1993 | 983 mm | 17.7 kg | tungsten alloy | 6.2 kg |  | 1501 m/s |  | 3.4 kg / 5.8 kg | 430 mm at 2000 m |  |
| M9718 |  South Africa | Denel |  | 950 mm | 18.5 kg | tungsten alloy |  | 350 to 400 MPa |  |  |  | 450 mm at 3000 m |  |
| K270 |  South Korea | Poongsan Corporation and Daewoo Corporation | 1980s |  |  | tungsten alloy |  |  | 1508 m/s | 52 m/s | / 5.36 kg | 152 mm at 60° obliquity at 3000 m |  |
| K273 |  South Korea | Poongsan Corporation and Daewoo Corporation | late 1980s or early 1990s |  |  | tungsten alloy |  |  |  |  |  |  | The K273 penetrator has a greater diameter-to-length ratio than the one of the K270. |
| K274 |  South Korea | Poongsan Corporation | 1998 | 1001 mm | 18.7 kg | tungsten alloy | M30 | 461.9 MPa | 1495 m/s |  | / 6.23 kg | 225 mm at 60° obliquity at 2000 m 480 mm at 3000 m |  |
| K274N |  South Korea | Poongsan Corporation | 2002 |  |  | tungsten alloy (2.4 kg) | SCDB |  | 1550 m/s |  |  | >500 mm at 60° obliquity at 2000 m |  |
| 105 mm FSAPDS |  India | Indian Ordnance Facotry Board (designer) and Ordnance factory of Khamaria Complex (producer) | 1996 |  |  | tungsten alloy | 4.3 kg or 5.1 kg |  | 1450 m/s |  | / 6.3 kg | 150 mm at 60° obliquity at 1300 m |  |
| APFS DS 105mm |  Pakistan | National Development Complex (NDC) | 2001 |  |  | depleted uranium |  |  | 1450 m/s |  |  | more than 450 mm at unknown range |  |
| P1A1 |  Pakistan | Pakistan Ordnance Factories (POF) |  |  |  | tungsten alloy | 5.62 kg of NQM046 | 434 MPa | 1490 m/s |  | 3.59 kg / 6.12 kg | 300 mm at 0° obliquity at unknown range | Licensed version of the British L64 APFSDS. |
| DTW2 |  China | NORINCO | before 2006 | 1066 mm | 18.8 kg | tungsten alloy | 5.9 kg of SD16 + SD16A | 511 MPa (max) | 1530 m/s |  | 3.775 kg / 6 kg | 150 mm at 71° obliquity at 2000 m | Also known under 105-II designation. |
| BTA2 |  China | NORINCO |  | 1100 mm | 18.8 kg | tungsten alloy | 5.8 kg |  | 1540 m/s | 40 m/s (at 1000 m) | / 5.9 kg | 220 mm at 66° obliquity at 2000 m | BTA2 is an export designation. |
| Anti tank 105 mm APFSDS – T |  Iran | Defense Industries Organization (DIO) | 2010s |  | 19 kg | tungsten alloy |  |  |  |  | / 5.3 kg | 460 mm at unknown range |  |