A Survey of Potential Ceramic Armor Materials, Revisited
In March 1968, 1st Lt. Jacob J. Stiglich, Jr. of the U.S. Army Materials and Mechanics Research Center (AMMRC) published A Survey of Potential Ceramic Armor Materials (AMMRC MS 68-04), a screening study compiled right after the first generation of monolithic alumina, silicon carbide, and boron carbide aircrew and personnel armor plates were fielded.
The primary aim of the study was to thoroughly document the range of materials that might be useful in future ceramic and ceramic-metal composite armor systems, and to then use that data to inform research into production. In most cases this was done on prototype scales. Unfortunately, you’ll notice that it didn’t result in anything to displace the three armor ceramics mentioned above.
But the original table is still useful, and I feel that it could do with a modern refresh. Before getting right into it, though, I’d like to highlight what I think you ought to look out for:
Promising Research Directions
Doped and boron-rich boron carbide (P2-CA-06, P2-CA-07): Small additions of silicon or a higher boron-to-carbon ratio modify the atomic chains between the B12 and B11C icosahedra that make up boron carbide’s crystal structure. This change mitigates amorphization at high pressure without significantly increasing density. A fully amorphization-resistant doped boron carbide has not yet been developed, but it doesn’t need to be fully resistant for use in body armor — it only needs to resist amorphization up to ~30GPa to defeat the tungsten-cored AP rounds in service today. (I’ll be writing another post about this soon.)
Multi-phase carbide and boride composites (P2-CA-04, P2-CA-05, P2-BO-01, P2-BO-03): Combinations of B4C, SiC, TiB2, AlB12, and potentially MgB2 have desirable properties. At a low density, and a low cost, they can be tuned for enhanced fracture toughness, amorphization resistance, and compressive strength. They can also exhibit multi-scale structural features: Widely-dispersed secondary phases keep the grains small during sintering, lock in compressive stresses on cooling, and stop cracks during impact.
Other icosahedral boron-rich ceramics (S1968-023, P2-BO-02, P2-BO-04): Boron suboxide B6O, boron subphosphide B12P2, and the aluminum magnesium boride AlMgB14 have densities of approximately 2.6 g/cm³ and hardnesses of 25-35 GPa. They have been of considerable institutional research interest for the past 15 or so years. Their current status is questionable, however, as B6O and B12P2 are unavoidably expensive to produce, and AlMgB14 has shown poor results in ballistic experiments [154].
Diamond and cubic boron nitride composites (P2-DI-01, S1968-069): Polycrystalline diamond, diamond-SiC, and various cBN composites are dense, generally much denser than boron carbide, but they also have superlative mechanical properties: Extreme hardness, extreme strength, and remarkable toughness. How to best utilize them and manufacture them is an open question in 2026, but diamond engineering is advancing at a remarkable pace, so I expect a meaningful update within the next few years.
In 1968, Stiglich looked for a single-phase ceramic with low density, high Young’s modulus and high hardness. Boron carbide had the best combination of these properties, and it was the high-end standard for almost 60 years. Static density, modulus and hardness are still the first filter for new candidate materials. However, the next improvement in ceramic armor doesn’t look like it’s going to come from a new two-element compound. The surer way to bet is that it’s going to come from doped lattices, engineered multi-phase composites, and eventually diamond-enhanced ceramics.
The table scrolls sideways and down inside its box. Download the full data (CSV) from Zenodo. It includes the 1968 values in their original units.
| Material | Formula | Density g/cm³ | Young’s modulus GPa | Hardness GPa | Hardness test | Values from | Availability | Sources |
|---|---|---|---|---|---|---|---|---|
| Part 1: The 1968 Survey | ||||||||
| Borides | ||||||||
| Silicon hexaboride | SiB6 | 2.43 | 414 | 19.6–23.5 | Knoop, 100 g | 1968 survey | Catalog item only (made to order) | 1; availability 2 |
| Various hexaborides | CaB6, SrB6, BaB6 | 2.46–4.32 | — | 26.5–29.4 | Knoop, 100 g | 1968 survey | Catalog item only (made to order) | 1; availability 3 |
| Beryllium boride | BeB2 | 2.403 | — | — | — | Calculated from crystal structure | Research only (calculations show cubic BeB2 is metastable; no bulk material) | 1, 4; availability 5 |
| Titanium diboride | TiB2 | 4.5 ± 0.1 | 565 | 25 | Vickers, 5 N | NIST recommended values (2000) | Powder sold (sintering grades); dense parts are special items | 1, 6; availability 7 |
| Various borides of Sc and Y | YB2, ScB2, YB3, YB4, YB6 | 2.91–4.36 | — | 25.8 (ScB2) 32.0 (YB6) | Knoop, 100 g | 1968 survey | Powder only (catalog item) | 1; availability 8 |
| Various borides of Al | AlB10; alpha-AlB12, beta-AlB12, gamma-AlB12 | 2.56–3.16 | — | 9.8–26.5 | Knoop, 100 g | 1968 survey | Catalog item only (AlB12); AlB10 not found | 1; availability 9 |
| Carbides | ||||||||
| Beryllium carbide | Be2C | 2.44 | 317 | 26.5 | Knoop, 100 g | 1968 survey | Catalog item only (made to order) | 1; availability 10 |
| Aluminum carbide | Al4C3 | 2.99 | — | — | — | 1968 survey | Powder only (catalog item) | 1; availability 11 |
| Boron carbide | B4C | >2.48 | 410 | 26 | Vickers HV1 | 3M grade (2015) | Commercial, dense parts (also armor) | 1, 12; availability 13 |
| Silicon carbide | SiC | >3.18 | 430 | 24.5 | Vickers HV1 | 3M F plus grade (2015) | Commercial, dense parts | 1, 14; availability 14 |
| Scandium carbide | ScC | 3.06 | — | 26.5 | Knoop, 100 g | 1968 survey | Catalog item (ScC2 found; ScC not found) | 1; availability 15 |
| Titanium carbide | TiC | 4.84–4.90 | 444–489 | 26–31 | Vickers (load not given) nanoindentation, 50 mN | Lab studies (2014–2018) | Powder and targets sold; dense parts are mostly cermets | 1, 16, 17, 18; availability 19 |
| Boron-doped SiC (1968 footnote) | SiC doped with B | >3.18 | 430 | 24.5 | Vickers HV1 | 3M F plus grade (2015) | Commercial, dense parts | 1, 14; availability 14 |
| Nitrides | ||||||||
| Beryllium nitride | Be3N2 | 2.71 | — | — | — | 1968 survey | Powder only (price on request) | 1; availability 20 |
| Magnesium nitride | Mg3N2 | 2.06 | — | — | — | 1968 survey | Powder only | 1; availability 21 |
| Alpha calcium nitride | alpha-Ca3N2 | 2.06 | — | — | — | 1968 survey | Powder only | 1; availability 22 |
| Strontium nitride | Sr3N2 | — | — | — | — | 1968 survey | Powder only | 1; availability 23 |
| Boron nitride (hexagonal) | BN (hexagonal) | 2.27 | — | 2.9 | Knoop, 100 g | 1968 survey | Commercial, dense parts | 1; availability 24 |
| Aluminum nitride | AlN | 3.2 | 310 | 11.2 | Vickers HV0.5 | Commercial grade | Commercial, dense parts | 1, 25; availability 13 |
| Silicon nitride | Si3N4 | 3.2 | 320 | 14.71 | Vickers HV0.5 | CeramTec grade | Commercial, dense parts | 1, 26; availability 13 |
| Cubic boron nitride (1968 footnote) | cubic BN | 3.45 | 909 (single crystal, calculated) | ≈40 | Vickers, load not given | Review value (PcBN) | Commercial, dense parts (tool blanks) | 1, 27, 28, 29, 30; availability 31 |
| Single Oxides | ||||||||
| Alumina | Al2O3 | 3.79–3.95 | 330–392 | 17.5 | Vickers HV0.2 (99.5% grade) | High-purity grades (1999 compilation; 2014 lab) | Commercial, dense parts (also armor) | 1, 32, 33; availability 13 |
| Beryllium oxide | BeO | 2.7–3.0 | 276 (90% dense) 414 (100% dense) | 17.6–21.6 | Knoop, 100 g | 1968 survey | Commercial, dense parts | 1; availability 34 |
| Magnesium oxide | MgO | ≈3.6 | 276 (90% dense) 379 (100% dense) | 7.8 | Knoop, 100 g | 1968 survey | Commercial, dense parts | 1; availability 35 |
| Boron suboxide | B6O | ≈2.6 | — | 33 | Method and load not given | Lab study (2009) | Research only | 1, 36; availability 37 |
| Calcium oxide | CaO | 3.2 | 114 | 5.9 | Knoop, 100 g | 1968 survey | Powder sold; dense parts not found | 1 |
| Continuous single-crystal sapphire filaments (1968 footnote) | Al2O3 (sapphire) | 3.97–3.98 | 344–420 | 19.6–21.6 | Knoop, 200 g | Surmet grade (single crystal) | Commercial (optical sapphire fibers) | 1, 38; availability 39 |
| Continuous single-crystal ruby filaments (1968 footnote) | Al2O3 (ruby; dopant not specified in report) | — | — | — | — | 1968 survey | Not found | 1 |
| Mixed Oxides | ||||||||
| Mullite (a complex silicate) | Mullite (no formula specified) | 2.5–3.0 | 137.9 | 5.9–11.8 | Knoop, 100 g | 1968 survey | Commercial, dense parts | 1; availability 40 |
| Many silicates (unspecified) (1968 footnote) | Not specified | <3.0 | — | — | — | 1968 survey | Not examined (no specified material) | 1 |
| Silicides | ||||||||
| Magnesium silicide | Mg2Si | 2.00 | — | — | — | 1968 survey | Powder and evaporation granules only | 1; availability 41 |
| Calcium silicide | Ca2Si | — | — | — | — | 1968 survey | Research only | 1; availability 42 |
| Calcium silicide | CaSi | 3.21 | — | — | — | 1968 survey | Not found | 1 |
| Calcium silicide | CaSi2 | 2.41 | — | — | — | 1968 survey | Powder only (technical-grade alloy) | 1; availability 43 |
| Strontium silicide | SrSi | 3.47 | — | — | — | 1968 survey | Not found (SrSi2 is sold) | 1; availability 44 |
| Barium silicide | BaSi2 | 3.98 | — | — | — | 1968 survey | Catalog item only (made to order) | 1; availability 45 |
| Boron-silicon compound | B4Si | 2.46 | — | 23.54 | Knoop, 100 g | 1968 survey | Powder only | 1, 46; availability 47 |
| Boron-silicon compound | B3Si | 2.64 | — | — | — | 1968 survey | Research only | 1, 46; availability 48 |
| Metalloid Elements | ||||||||
| Boron | B | 2.3–2.5 (various allotropes) | 228 | 31.0 ± 1.8 | Vickers HV1 | Hardness: lab study; density and E: 1968 survey | Powder only | 1, 49 |
| Silicon | Si | 2.3–2.55 | 103–110 | 6.9 | Knoop, 100 g | 1968 survey | Commercial, dense parts (IR optics) | 1; availability 50 |
| Germanium | Ge | 5.3–5.8 | 159 (single crystal <111> direction) | 6.9 | Knoop, 100 g | 1968 survey | Commercial, dense parts (IR optics) | 1; availability 51 |
| Metalloid Compounds | ||||||||
| Beryllium phosphide | Be3P2 | 2.06 | — | — | — | 1968 survey | Catalog item only (made to order) | 1; availability 52 |
| Magnesium phosphide | Mg3P2 | 2.02 | — | — | — | 1968 survey | Commercial only as fumigant pellets (these release phosphine) | 1; availability 53 |
| Barium phosphide | Ba3P2 | 3.18 | — | — | — | 1968 survey | Powder only (catalog item) | 1; availability 54 |
| Boron phosphide | BP | 2.976 | 362 ± 36 | 29 ± 2 | Vickers, ≥4 N | Lab study (2019) | Research only (small high-pressure pieces) | 1, 55; availability 56 |
| Aluminum phosphide | AlP | — | — | — | — | 1968 survey | Commercial only as fumigant tablets (these release phosphine) | 1; availability 57 |
| Scandium phosphide | ScP | 3.28 | — | — | — | 1968 survey | Catalog item only (made to order) | 1; availability 58 |
| Antimonides (unspecified) (1968 footnote) | Not specified | — | — | — | — | 1968 survey | Semiconductor targets and wafers only | 1; availability 59 |
| Bismuthides (unspecified) (1968 footnote) | Not specified | — | — | — | — | 1968 survey | Not found | 1 |
| Intermetallic Compounds (Beryllides) | ||||||||
| Titanium beryllide | TiBe2 | 3.23 | — | — | — | 1968 survey | Not found | 1 |
| Titanium beryllide | TiBe12 | 2.3 | — | 9.4 | Knoop, 2.5 kg | 1968 survey | Research only (fusion blanket studies) | 1; availability 60 |
| Zirconium beryllide | Zr2Be17 | 3.05 | 310 | 11.1 | Knoop, 2.5 kg | 1968 survey | Not found | 1 |
| Zirconium beryllide | ZrBe13 | 2.72 | 324 | 9.8 | Knoop, 2.5 kg | 1968 survey | Not found | 1 |
| Vanadium beryllide | VBe12 | 2.35 | — | — | — | 1968 survey | Not found | 1 |
| Niobium beryllide | Nb2Be17 | 3.28 | 296 (dynamic) 331 (static) | 9.8 | Knoop, 2.5 kg | 1968 survey | Research only (Be17Nb2 occurs in Be12Nb studies) | 1; availability 61 |
| Niobium beryllide | Nb2Be19 | 3.15 | — | — | — | 1968 survey | Not found | 1 |
| Niobium beryllide | NbBe12 | 2.91 | 324 | 4.9 | Knoop, 2.5 kg | 1968 survey | Research only | 1; availability 61 |
| Tantalum beryllide | Ta2Be17 | — | 193 (dynamic) 372 (static) | — | — | 1968 survey | Not found | 1 |
| Molybdenum beryllide | MoBe12 | 3.03 | — | 9.3 | Knoop, 2.5 kg | 1968 survey | Not found | 1 |
| Tungsten beryllide | WBe22 | 3.23 | — | — | — | 1968 survey | Not found | 1 |
| Cermets | ||||||||
| SiC + 35% Vitallium by volume | SiC + 35 vol% Vitallium | 3.13 (13.6% porosity) | — | — | — | 1968 survey | Not found | 1 |
| 70 Al2O3 / 30 Cr (wt %) | 70 wt% Al2O3 + 30 wt% Cr | 4.6–4.65 | 359 | ≈14.7 | Knoop, 100 g | 1968 survey | Research only (other Al2O3-Cr compositions) | 1; availability 62 |
| B4C-Fe bonded (36.4% Fe) | B4C-Fe (36.4% Fe) | 3.24 | 359 | ≈14.7 | Knoop, 100 g | 1968 survey | Research only | 1; availability 63 |
| BeO-Be bonded (8% Be) | BeO-Be (8% Be) | 2.86 | 359 | ≈14.7 | Knoop, 100 g | 1968 survey | Not found with 8% Be; BeO/Be with 20–60% BeO is sold (price on request) | 1; availability 64 |
| SiO2-Al bonded | SiO2-Al | — | 359 | ≈14.7 | Knoop, 100 g | 1968 survey | Not found. Al reacts with silica and makes Al2O3. | 1; availability 65 |
| TiC cermets (0 to 50 wt % Co or Ni) | TiC + 0 to 50 wt% Co or Ni | 5.5–6.8 | 310–379 | HRA 85–90 | Rockwell A | 1968 survey | Commercial, dense parts (TiC-TiN-Mo-Ni cermets) | 1; availability 66 |
| Composites | ||||||||
| TiC with additions of ZrB2 or TiB2 or Mo2C (1968 footnote) | TiC-ZrB2; TiC-TiB2; TiC-Mo2C | — | — | — | — | 1968 survey | Not examined | 1 |
| SiC-silicon nitride bonded | SiC-silicon nitride bonded | 2.5–2.8 (13–15% porosity) | 117 | — | — | 1968 survey | Commercial, dense parts (refractories) | 1; availability 67 |
| SiC-silicon oxynitride bonded | SiC-silicon oxynitride bonded | ≈2.7 (≈18% porosity) | 117 | — | — | 1968 survey | Not found with an oxynitride bond; SiC with a nitride or oxide bond is sold | 1; availability 67 |
| SiC + graphite | SiC + graphite | 2.3–2.8 (8–26% porosity) | 241 | — | — | 1968 survey | Commercial, dense parts (seals, bearings) | 1; availability 68 |
| Alclad B4C | Alclad B4C | 2.5 | — | — | — | 1968 survey | Commercial equivalent: Al-clad Al-B4C neutron-absorber plate | 1; availability 69 |
| Cr-reinforced Al2O3 (30 wt % Cr) | Cr-reinforced Al2O3 (30 wt% Cr) | 4.6–4.65 | 360.6 | 10.8–11.8 | Knoop, 100 g | 1968 survey | Research only (other Al2O3-Cr compositions) | 1; availability 62 |
| Oxide “Alloys” | ||||||||
| Al2O3·P2O5 (melting point 2900 F) | Al2O3·P2O5 | 2.6 | — | — | — | 1968 survey | Powder only | 1; availability 70 |
| Al2O3·MgO | Al2O3·MgO | 3.6 | 241 | 11.8–13.7 | Knoop, 100 g | 1968 survey | Commercial as spinel (refer to Part 2) | 1 |
| Part 2: Added Since 1968 | ||||||||
| Borides and Boron-Rich Compounds | ||||||||
| Al-B-C composite with 10 vol% TiB2 | AlB12-AlB12C2-10vol%TiB2 | 2.76 | — | 37 | Vickers, load not given | Lab study (2020) | Research only | 71 |
| Aluminum magnesium boride (BAM) | AlMgB14 | ≈2.6 | — | 25–35 | Method and load not given | Modern range | Research only (published ballistic studies) | 72, 73 |
| BAM with 15 wt% TiB2 and 15 wt% HfC additions | AlMgB14 + 15wt%TiB2 + 15wt%HfC | 3.22 | — | 25.3 | Vickers HV1 | Lab study (2025) | Research only | 74 |
| Boron subphosphide | B12P2 | 2.589 | 454 ± 23 | 35 ± 2 | Vickers, ≥3 N | Lab study (2019) | Research only | 55 |
| Magnesium diboride | MgB2 | 2.666 | 245–273 | 10.4–11.7 | Vickers HV1 | Lab study (2002), HIP | Powder sold; no armor-grade dense parts | 75, 76 |
| Aluminum diboride (thin film) | AlB2 | — | 332 ± 14 | 19.2 ± 1.2 | Nanoindentation (film) | Lab study (2025), thin film | Powder sold; dense parts in research only | 77 |
| Zirconium diboride | ZrB2 | 6.08 | 529 ± 17 | 15.3 ± 0.5 | Vickers HV1 | Lab study (2023) | Commercial, dense parts | 78 |
| Hafnium diboride | HfB2 | 10.7 | 560–580 | 26–28 | Nanoindentation, 500 mN | Lab study (2008) | Powder sold; dense parts made to order | 79 |
| Chromium diboride | CrB2 | 5.05 | 422 | 12.3 | Vickers, 0.49–9.8 N asymptote | Lab study (2025) | Powder sold; dense parts in research only | 80 |
| Niobium diboride | NbB2 | — | 542 ± 13 | — | — | Lab study (2017) | Powder sold; dense parts in research only | 81 |
| Tantalum diboride | TaB2 | 11.96 | 571 ± 13 | 20.7 ± 0.8 | Vickers HV1 | Lab study (2016) | Powder sold; dense parts in research only | 82 |
| Rhenium diboride | ReB2 | — | — | 29.3 ± 0.8 | Vickers, 4.9 N | Lab study (2016), arc-melted | Research only | 83 |
| Tungsten tetraboride | WB4 | — | — | ≈43 | Vickers, 0.49 N | Lab study (2015), arc-melted | Research only | 84 |
| Chromium tetraboride | CrB4 | — | — | ≈30 | Vickers asymptote, load not given | Lab study (2014) | Research only | 85 |
| Boron subnitride | B13N2 | — | 515 ± 16 | 41 ± 2 | Vickers, 1–6 N asymptote | Lab study (2017) | Research only (mm-size pieces) | 86 |
| Boron subarsenide | B12As2 | — | — | ≈31 | Vickers, load not given | Lab study (2022) | Research only | 87, 88 |
| Cubic boron carbonitride | c-BC2N | — | — | 76 | Vickers, load not given | Lab study (2001) | Research only (mm-size pieces) | 28 |
| Carbides and Carbide Composites | ||||||||
| Liquid-phase-sintered / toughened SiC example | SiC-YAG | >3.24 | 430 | 22.5 | Vickers HV1 | 3M T plus grade (2015) | Commercial | 14 |
| Reaction-bonded silicon carbide | SiC-Si | 3.09 | 362.39 | 19.43 | Method and load not given | Lab study (2006) | Commercial | 89 |
| Reaction-bonded boron carbide | B4C-SiC-Si | ≈2.53–2.66 (calculated) | 330–430 | 16–29 | Vickers, load not given | Lab study (2017) | Commercial (armor) | 90 |
| Dense boron-carbide / silicon-carbide composites | B4C-SiC | 2.55–3.20 | — | — | — | Estimated range (see note) | Commercial, special items and research | 91 |
| Boron-carbide / titanium-diboride composites | B4C-TiB2 | 2.6–3.2 | — | 27.3–28.4 | Vickers HV1 | Estimated range (see note) | Research and special items | 92, 93 |
| Silicon-doped boron carbide | B4C with approximately 1at%Si | — | — | — | — | Lab study (2019) | Research and special items | 94, 95 |
| Boron-rich boron carbide | B-rich B-C solid solution | — | — | — | — | Material family | Research and special items | 96 |
| Zirconium carbide | ZrC | 6.66 | 402 ± 13 | 17.5 ± 0.4 | Vickers HV1 | Lab studies (2016, 2018) | Powder sold; dense parts in research or made to order | 17, 97, 98 |
| Hafnium carbide | HfC | 12.52 | 428 ± 32 | 25 ± 2 | Nanoindentation, 50 mN | Lab study (2018) | Powder sold; dense parts in research only | 17, 98 |
| Niobium carbide | NbC | 7.79 | 429 ± 46 | 17 ± 3 | Nanoindentation, 50 mN | Lab study (2018) | Powder sold; dense parts in research only | 17, 99 |
| Tantalum carbide | TaC | 14.5 | 431 ± 44 | 14 ± 2 | Nanoindentation, 50 mN | Lab study (2018) | Powder sold; dense parts in research only | 17, 99 |
| Vanadium carbide | VC | — | 465 ± 13 | 29 ± 1 | Nanoindentation, 50 mN | Lab study (2018) | Powder sold (hardmetal additive) | 17, 100 |
| Tungsten carbide, binderless | WC | ≈15.56 | — | 26.7 | Vickers HV10 | Lab study (2013) | Commercial, dense parts for special applications | 101 |
| Silicon carbide-titanium diboride composite | SiC + 15 vol% TiB2 | 3.36 | 413 | — | — | Commercial grade (Hexoloy ST, 1997 data) | Commercial before; current supply not found | 102 |
| Silicon carbide-aluminum nitride composite | (SiC)1-x(AlN)x | — | — | 12.5–29.8 (by composition) | Vickers, 4.9 N | Lab study (approximately 1990) | Research only | 103 |
| Nitrides and Oxynitrides | ||||||||
| SiAlON, beta grade | β-SiAlON (Syalon 101) | 3.24 | 288 | 14.7 | Vickers HV50 | Syalons grade | Commercial, dense parts | 104 |
| Nano-polycrystalline cubic BN, binderless | cBN | — | — | 43.6–46.0 | Knoop, load not given | Lab study (2014) | Commercial (tool blanks) | 105 |
| Nanocrystalline cubic BN (10–50 nm grains) | cBN | — | 961 ± 39 | 63 ± 2 | Knoop, 5 N asymptote | Lab study (2019) | Research only | 29 |
| SiAlON, alpha/beta grade | α/β-SiAlON (Syalon 050) | 3.23 | 290 | 19.8 | Vickers HV50 | Syalons grade | Commercial, dense parts | 106 |
| Titanium nitride | TiN | 5.16 | 370 | 23.2 ± 1.0 | Microhardness, method not given | Lab study (2009) | Powder sold; dense parts in research only | 98, 107, 108 |
| Zirconium nitride (single-crystal film) | ZrN | 7.14 | 450 | 22.7 ± 1.7 | Method not given | Lab study (2013), epitaxial film | Powder sold; dense parts in research only | 98, 109 |
| Silicon oxynitride | Si2N2O | 2.83 | 217 | 15.2 | Vickers HV10 | Lab study (1980) | Research only | 110 |
| Oxides | ||||||||
| Zirconia-toughened alumina | Al2O3-ZrO2 | 4.0–4.3 | 335–380 | 14.4–18.4 | Vickers HV0.5–HV1 | Commercial grades | Commercial | 111, 112, 113 |
| Magnesium aluminate spinel | MgAl2O4 | 3.58 | 271 | — | — | Commercial grade | Commercial | 114 |
| Aluminum oxynitride | AlON | 3.69 | 334 | 18.14 | Knoop, 200 g | Commercial grade | Commercial | 38 |
| Yttria-stabilized zirconia (3Y-TZP) | ZrO2 + 3 mol% Y2O3 | 6.07 | 205 | 12.8 | Vickers HV0.3 | Morgan grade | Commercial, dense parts | 115 |
| Magnesia-partially-stabilized zirconia (Mg-PSZ) | ZrO2 + 3.5 wt% MgO | 5.74 | 205 | 10.0 | Vickers HV0.3 | Morgan grade | Commercial, dense parts | 116 |
| Yttria, transparent | Y2O3 | 5.03 | 176 | 8.8 | Vickers, load not given | Lab study (2010) | Commercial, dense parts (IR windows) | 117, 118 |
| Yttrium aluminum garnet (YAG), transparent | Y3Al5O12 | 4.55 | 297 | 12.6 | Vickers HV10 | Lab studies (2018; Ikesue) | Commercial, dense parts (laser optics) | 119, 120 |
| YAG-alumina transparent nanoceramic | Y3Al5O12 + Al2O3 | 4.25 | 281 | 23.6 | Nanoindentation, 600 mN | Lab study (2018) | Research only | 119 |
| SiC-whisker-reinforced alumina | Al2O3 + 20 wt% SiC whiskers | — | 420 (calculated) | 18.4 | Vickers HV3 | Lab study (2006) | Commercial, dense parts (cutting tools); armor use is in research | 121 |
| Glasses and Glass-Ceramics | ||||||||
| Soda-lime float glass (low-iron) | Soda-lime-silica | 2.51 | 73.1 | 4.6 | Knoop, 500 g | Vitro grade | Commercial, dense parts | 122 |
| Borosilicate glass | SiO2-B2O3 (SCHOTT Borofloat 33) | 2.23 | 64 | 4.7 | Knoop, 100 g | SCHOTT grade | Commercial, dense parts | 123 |
| Fused silica | SiO2 | 2.201 | 72.7 | 5.1 | Knoop, 100 g | Corning grade | Commercial, dense parts | 124 |
| Chemically strengthened aluminosilicate glass | Alkali aluminosilicate (Corning Gorilla Glass 3) | 2.39 | 70 | 6.4 (strengthened) 5.4 (unstrengthened) | Vickers, 200 g | Corning grade | Commercial, thin sheet | 125 |
| Lithium aluminosilicate glass-ceramic | Li2O-Al2O3-SiO2 (SCHOTT Zerodur) | 2.53 | 90.3 | 6.1 | Knoop, 100 g | SCHOTT grade | Commercial, dense parts | 126 |
| Transparent glass-ceramic (Corning) | Corning Gorilla Glass Ceramic | 2.47 | 102 | 6.4 (strengthened) 6.2 (unstrengthened) | Knoop, 200 g | Corning grade | Commercial, dense parts | 127 |
| Transparent lithium-disilicate glass-ceramic | Li2Si2O5-based (TransArm) | 2.5–2.8 | 95–115 | 6–7 | Vickers, load not given | Secondary source | Commercial, small quantities | 128 |
| Transparent MAS glass-ceramic | MgO-Al2O3-SiO2 | 2.6 | 96.5 | 8.9 | Vickers, load not given | Lab study (CSIR-CGCRI) | Research only | 128 |
| Diamond | ||||||||
| Diamond-silicon-carbide composite | Diamond-SiC | — | — | — | — | Material family | Research and special items | 129 |
| Polycrystalline diamond (PCD), cobalt-bonded | Diamond + Co | — | 841 | 49.8 | Knoop, load not given | US Synthetic grade | Commercial, small compacts | 130 |
| CVD diamond, polycrystalline | C | 3.52 | 1050 | 81 ± 18 | Method not given | Element Six grade | Commercial, wafers and windows | 131 |
| Binderless nano-polycrystalline diamond | C | — | — | 110–140 | Knoop, 4.9 N | Lab study (2003, 2008) | Research only (small pieces) | 132, 133 |
| Cermets and Metal-Ceramic Composites | ||||||||
| Boron-carbide / aluminum cermet | B4C-Al | — | — | — | — | Material family | Research and special items | 134 |
| Aluminum-dodecaboride / aluminum cermet | AlB12-Al | — | — | — | — | Material family | In development | 134, 135 |
| Alumina-reinforced aluminum (cast MMC) | Al-4Mg + 46 vol% Al2O3 | 3.30 | 160 | — | — | Lab study (2013) | Commercial | 136 |
| Silicon-carbide-reinforced aluminum, armor grade | Al-10Si + 55 vol% SiC | 2.96 | 202 | — | — | Lab study (2013) | Commercial | 136 |
| SiC fiber / SiC matrix composite | SiC/SiC | 2.51 | 252 (in-plane) | — | — | Lab studies (2005, 2009) | Commercial (aerospace) | 137, 138 |
| Carbon fiber / SiC matrix composite | C/SiC (short-fiber) | 2.65 | 250 | — | — | Commercial grade (1999) | Commercial (optics, brakes) | 139 |
| Cemented carbide (WC-6% Co) | WC-6Co | 14.95 | 600 | 15.2 | Vickers, load not given | Goodfellow grade | Commercial, dense parts | 140, 141 |
| Titanium diboride with nickel | TiB2 + 0.25-3 wt% Ni | 4.50–4.62 | 514–574 | 22–24 | Vickers, 5.65 N | Lab study (1983, NIST data) | Research only | 142 |
| Titanium carbonitride cermet | Ti(C,N) + alloyed binder | 6.7–7.3 | — | 14.7–15.2 | Vickers HV30 | Hyperion grades | Commercial, dense parts | 143 |
| MAX Phases and Silicides | ||||||||
| Titanium silicon carbide | Ti3SiC2 | ≈4.5 | ≈320 | ≈4 | Vickers, 100 N | Review compilation (2024) | Powder sold; few dense parts | 144, 145 |
| Titanium aluminum carbide (211) | Ti2AlC | 4.1 | — | — | — | Review compilation; Kanthal grade | Commercial (Kanthal) | 144, 146 |
| Titanium aluminum carbide (312) | Ti3AlC2 | 4.21 | 297 | 2.7–3.5 | Method not given | Review compilation | Powder sold | 144, 147 |
| Chromium aluminum carbide | Cr2AlC | 5.17 | ≈282 | ≈4.9 | Method not given | Review compilation | Powder sold | 144, 147 |
| Molybdenum disilicide | MoSi2 | 6.23 | 440 | 9.6 | Vickers, 148 N | Lab study (2004) | Commercial, dense parts (heating elements) | 148, 149 |
| Titanium disilicide | TiSi2 | 4.09 | 256 | — | — | Lab study (1992) | Powder sold | 150 |
| High-Entropy Ceramics | ||||||||
| Five-metal high-entropy diboride | (Hf0.2Zr0.2Ti0.2Ta0.2Nb0.2)B2 | 8.25 | — | 20.5 ± 1.0 | Vickers HV0.2 | Lab study (2020) | Research only | 151 |
| Mo-containing five-metal high-entropy diboride | (Hf0.2Zr0.2Ti0.2Ta0.2Mo0.2)B2 | 8.35 | — | 24.9 ± 1.0 | Vickers HV0.2 | Lab study (2020) | Research only | 151 |
| Cr-containing five-metal high-entropy diboride | (Hf0.2Zr0.2Ti0.2Ta0.2Cr0.2)B2 | 7.83 | — | 24.9 ± 1.0 | Vickers HV0.2 | Lab study (2020) | Research only | 151 |
| Six-metal high-entropy diboride | (Hf1/6Mo1/6Nb1/6Ta1/6W1/6Zr1/6)B2 | 8.98 | 520 ± 12 | 33.1 ± 1.1 | Vickers HV0.2 | Lab study (2022) | Research only | 152 |
| Five-metal high-entropy carbide | (Hf0.2Nb0.2Ta0.2Ti0.2Zr0.2)C | — | 443 ± 40 | 32 ± 2 | Nanoindentation, 50 mN | Lab study (2018) | Research only | 153 |
How to Read This Table
- Part 1 and Part 2
- Part 1 has all the materials in the 1968 table of Stiglich, in his categories. It also has the materials that his footnotes name. Part 2 has the materials that are not in the 1968 survey. These are new process variants and composites, materials that the 1968 survey did not include, and compositions that did not exist in 1968.
- Density
- The bulk density in g/cm³. A value with “>” is the minimum value that the manufacturer gives for that grade.
- Young’s modulus
- The stiffness in GPa. The 1968 survey gives these values in millions of psi. We converted them to GPa (1 Mpsi = 6.895 GPa) and rounded them to the nearest whole number.
- Hardness
- The hardness in GPa. The 1968 survey gives Knoop hardness in kgf/mm². We converted these values to GPa (1 kgf/mm² = 0.00981 GPa) and rounded them to one decimal place. The hardness value changes with the test method and the load. Do not directly compare Knoop values with Vickers values. Do not directly compare low-load values with high-load values. For this reason, read this column together with the next column. On the same material, nanoindentation gives values that are much higher than Vickers or Knoop values.
- Hardness test
- The indentation method and the load for the hardness value, when the source gives them.
- Values from
- “1968 survey” shows that the values are from Stiglich. We converted these values, but we did not measure them again. “Lab study” shows a value from one published specimen. This specimen is frequently small, and it is not a production plate. “Commercial grade”, or the name of a manufacturer with “grade”, shows the data sheet of one manufacturer. This value does not apply to all the material family. “Calculated” shows a value from the crystal structure or from theory. It is not a measurement on a bulk part.
- Availability
- The status in October 2026. We examined the pages of the manufacturers and suppliers. “Commercial, dense parts” shows that a company sells sintered or pressed shapes. “Powder only (catalog item)” shows that a catalog supplier lists the compound. Usually, the supplier makes it only when you order it. This does not show that a company makes dense parts from it. “Not found” shows that we found no current supplier and no recent research. The CSV file also gives the status that Stiglich printed in 1968.
- Sources
- The numbers are links to the list below. Source 1, the 1968 survey, applies to all Part 1 rows. A number after “availability” applies only to the Availability column. It does not apply to the property values.
- —
- The sources do not give a value.
The table includes beryllium compounds (beryllides, BeO, Be2C and other compounds) because Stiglich included them. The powders of these compounds are toxic. Use special procedures to handle them. Use the property values only to select and compare materials. They do not replace ballistic tests of a finished plate.
Dataset: Ganor, J. (2026). Ceramic Armor Materials, 1968 to 2026: An Updated Survey Dataset (Version 1.0) [Data set]. Zenodo. https://doi.org/10.5281/zenodo.23565137. The dataset has all 154 rows as a CSV file, with the 1968 values in their original units, the availability sources and a README.
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