1. Introduction
The development of counterattack and protection weapons against external threats has continued throughout human history. Emerging conflicts have driven humans to develop body armor to safeguard themselves against the effects of weapons. The armor system was introduced to provide the utmost protection against threats like stabbing, explosions, and high-impact penetration. Consequently, primitive materials such as leather, wood, and steel became popular for crafting both weapons and protective shields in the early stages [
1,
2]. Over time, the popularity of hard and soft body armor has increased with the rise of global conflicts. Soft body armor provides high flexibility and comfort, especially for lower NIJ threat levels. In contrast, hard body armor is typically made of ceramics, steel, or polyethylene, which are preferred for protection against high-velocity impacts. However, the use of these armors is often limited due to excessive weight and discomfort to the wearer. Therefore, various fabrics and laminates composed of traditional fibers, such as nylon and Kevlar, were introduced in the late 1939s for ballistic protection systems [
3]. Until the 1970s, nylon was accepted as a standard fiber and a ballistic material; however, other high-performance fabrics, such as para-aramid and ultra-high molecular weight polyethylene (UHMWPE), were introduced by DuPont in 1965 to further advance in the field [
4]. Para-aramid (Kevlar and Twaron) and UHMWPE (Spectra and Dyneema) are two well-known high-performance fabrics that researchers have investigated for high-impact-resistant applications [
4,
5]. Early researchers achieved protection by adding up to 40 fabric layers to meet body armor safety standards; however, this created a bulky design and reduced the wearer's flexibility [
7]. Researchers faced the primary challenge of minimizing weight and enhancing the flexibility of body armor without compromising its strength. They resolved these issues in the early 2000s by introducing shear-thickening fluids (STFs) [
8].
STF is a type of intelligent ballistic-resistant material that is composed of solid particles suspended in a dispersion medium [
9,
10]. STF exhibits non-Newtonian characteristics whose viscosity abruptly changes with increased shear rate. The fluid exhibits reversible behavior, transitioning from a liquid to a solid phase at high shear rates, making it a potential material for absorbing impact energy [
11,
12,
13]. Hence, this feature of STFs is used to impregnate high-performance fabrics, intended to boost the impact resistance of fabric under high-impact loading. Maximum attention is being given to soft body armor instead of hard armor due to its advantages for the wearer, as evidenced by current research trends in section 1.1.
The novelty of this review is reflected in its combined assessment of both material level and projectile level governing ballistic performance and at the same time integrating these fundamentals to the contemporary improvement techniques. Unlike previously reported reviews that focus narrowly on fabrics or testing standards, the current work correlates fabric architecture, assembly parameters, projectile attributes, and advanced reinforcement methods such as shear thickening fluids, latex coatings, and fiber modifications. Additionally, the review provides in depth analysis of emerging evaluation techniques namely, yarn friction, puncture resistance, ballistic limit velocity, and back- face signature. Thus, this review provides a comprehensive and layered analysis that helps the new researchers to understand the design and development of next-generation soft body armor.
1.1. Bibliometric Analysis
In the last 15 years, the keywords “body armor” and “body armour ” have yielded 1316 and 1699 research articles in the Web of Science database, respectively. However, only 259 of these specifically focus on “soft body armor,” indicating a novelty and a significant scope of research on this topic. The co-occurrence of keywords used in research by worldwide scholars and scientists is visualized in
Figure 1. Node size represents the frequency of each keyword. The large node size represents the most frequent keywords in the retrieved literature. It is clear from
Figure 1 that keywords such as body armor, ballistic impact, stab resistance, Kevlar, fumed silica, finite element analysis, and impact behavior have been the focus of previous studies.
The bar diagram (
Figure 2) represents the research outcomes for both soft and hard body armor from 2011 to 2025 A total of 1316 articles were published on body armor-related keywords. Researchers from countries such as the United States, China, the United Kingdom, and India have emerged as the leading contributors to body armor research, dominating the field's publication landscape. A bibliometric analysis (
Figure 3) using the Web of Science database reveals that these countries have consistently published several papers from 2011 to 2025 (as of 6 December 2025). For this analysis, only countries with at least three publications during this period were considered. The pictographic representation reflects global research trends in body armor technologies.
1.2. Advancement in STF
Further, the work was extended to STF-impregnated high-performance fabric for the development of lightweight, flexible armor. However, their use is limited due to key issues such as high cost, low STF retention, and non-biodegradability [
14]. Therefore, researchers have made efforts by hybridizing traditional fibers with naturally derived fibers [
15,
16,
17,
18,
19,
20]. Recently, STF-impregnated jute fabrics have been evaluated for their ballistic performance and puncture resistance. The findings of this research confirmed the potential of jute fabrics for developing sustainable protective armors and gears in the future [
21]. As the demand for soft body armor continues to rise, its year-by-year evolution is illustrated in
Figure 4, which shows that Kevlar and STF-treated Kevlar fabrics have been widely used for ballistic protection. However, from late 2018, the research community also began exploring natural fibers [
22,
23].
This review aims to provide an in-depth understanding of findings from worldwide researchers to design a soft body armor that can be effectively integrated into current scenarios. The article examines the historical evolution of body armor from ancient times, highlighting its benefits and limitations. The year-by-year development of armor materials and their performance under both low- and high-velocity impacts is discussed. Furthermore, parameters influencing impact energy absorption, including fiber properties, yarn parameters, fabric layers, ply arrangement, hybridization, and fabric structure, are discussed. Additionally, the review examines the impact of projectile geometry on the performance of fabric materials, providing an rigorous analysis of various testing standards. The underlying mechanism of STFs, as well as the influence of particle shape and size, volume fraction, hardness, roughness, and carrier medium, is explained. Emphasis is placed on the potential use of STF-impregnated naturally driven fabric and its characterization. It is believed that the current technology used in STF-impregnated synthetic fabric composites has the potential to be leveraged in the fabrication of natural fiber composites designed for ballistic applications. Hence, the article also provides the reader with deeper insight into STF-impregnated natural fiber composites and their applications in the design of protective systems.
1.3. Classification of Body Armor
The armor is classified as either hard (rigid) or soft, depending on the materials used to protect against various threats. The hard body comprises a metal, ceramic, and polyethylene layer, used mainly for high protection against high-velocity impact loads [
24]. On the contrary, soft body armor is constructed from several layers (generally 20-50) of high-performance fabric to achieve low to moderate ballistic protection [
25]. Despite offering high-level protection against ballistic impact loads, the demand for hard body armor has declined for threats from low-velocity impact over the last few decades due to its inflexibility and unfavourable weight-to-strength ratio. In contrast, high-performance synthetic fibers were found to provide excellent strength and modulus, as well as enhanced chemical resistance, compared to hard body armor [
7]. Recently, hybrid composites have emerged as a major focus of research in developing soft body armor owing to their enhanced impact resistance against threats such as stabbing, bullets, and shrapnel [
26]. A comprehensive discussion of the development of body armor materials is highlighted in
Section 1.4.
1.4. Evolution of Body Armor Materials
Over the centuries, humans have adopted various tactics to protect themselves from the environment, animals, and enemies. Depending on the threats, protection was ensured in multiple ways, such as seeking safe shelters to avoid proximal threats, fleeing for survival, and using protective shields and weapons to confront situations directly. Among all the tactics humans used, protective shields/armor were popularized as a personal protection system [
1]. In the advancement of human history, the Persians and Greeks acquired significant expertise in developing more sophisticated weapons, respectively, around 600 BC [
27]. The Persians used large bronze plates mounted on leather harnesses, while the Greeks used iron plates mounted on leather harnesses. Later, steel-plated armor was introduced during the medieval period of European history to achieve greater flexibility in combat. The steel-plated armor disappeared from infantry after the 18th century due to its ineffectiveness and weight against contemporary weapons. Besides metal protection systems, Chinese and Mongolian warriors used fabric armor, such as leather and animal skin, from the 11th to the 13th century CE [
28]. Moreover, quilted linen coats were used in northern India until the 19th century. Despite the advancement in protection systems, the devastating casualties faced by troops during World War I were as result of advanced weapons like machine guns, snipers, and shrapnel. Therefore, Coates and Bayers [
1] conducted a systematic study to investigate the impact of firearms on various parts of the body. They found that the lower and upper limbs were most affected, at 39% and 22%, respectively, followed by the chest at 16% and the head and neck at 12% [
29,
30].
During the later part of the Korean War, the US introduced the M-1952 (a model code name for a nylon-based body armor) [
31]. The flexible vest weighed 3.6 kg and consisted of 12 layers of laminated nylon, offering improved ballistic protection against shell fragments. Subsequently, they introduced M-1969 (a 15-layered nylon-based body armor) to attain high protection efficiency of the existing M-1952. The performance of nylon-based flexible vests has set a new benchmark for other fabrics to explore for their potential to resist ballistic threats [
32]. Therefore, researchers have begun exploring other synthetic fibers in their quest for improved ballistic resistance, reduced weight, and high tensile strength against various threats, which are elaborated upon in
Section 1.5.
1.5. Protection Against Different Types of Threats
Different kinds of body armor have been designed to safeguard against handguns, rifles, automatic weapons, sniper rifles, shrapnel, and stabbing attacks. Various types of body armor are classified according to their resistance to penetration by different bullets and calibers, as per the National Institute of Justice NIJ-0101.06 [
33]. Depending on threat level, troops can choose between soft and semi-rigid (a combination of fabric and metal) body armor. Shrapnel or fragments from an explosive can be harmful to humans, including sharp, small metal pieces that body armor can easily tackle [
34]. Several sharp, pointed stabbing tools, including domestic knives, utility knives, and spiking objects, have been in use by humans for single or multiple cutting, slashing, and piercing.
Ballistic armor is designed to protect the wearer against different threats. The armor must be lightweight and flexible for modern warfare [
35]. Fibrous body armor replaces hard body armor to achieve the highest comfort for the wearer without compromising the impact resistance performance [
36]. Nowadays, various technical textiles, such as Kevlar and UHMWPE fibers, are suitable for developing soft body armor. Modern armor also features cooling channels embedded in its structure to improve air circulation. It features attachment points for various components, including protection for the neck, shoulders, and upper and lower limbs [
37].
Figure 5 provides a detailed illustration of armor made from synthetic fibers.
Furthermore, the investigation began by analyzing the impact of energy-absorption phenomena in soft body armor through wave propagation in various high-performance fabrics.
Section 2 highlights the key investigation reported in previous studies.
Figure 1.
Network visualization map of keywords used by worldwide authors in their documents for body armor research from 2011-2025: (Web of Science data, assessed on 6 December 2025).
Figure 1.
Network visualization map of keywords used by worldwide authors in their documents for body armor research from 2011-2025: (Web of Science data, assessed on 6 December 2025).
Figure 2.
Number of articles published from 2011-2025 (Web of Science data, accessed on 6 December 2025).
Figure 2.
Number of articles published from 2011-2025 (Web of Science data, accessed on 6 December 2025).
Figure 3.
Network visualization map of research outcomes of top active countries with at least 3 articles on body armor.
Figure 3.
Network visualization map of research outcomes of top active countries with at least 3 articles on body armor.
Figure 4.
Year-by-year evolution in designing soft body armor.
Figure 4.
Year-by-year evolution in designing soft body armor.
Figure 5.
Soft body armor: (a) Nomenclature, (b) Neck protection, (c) Shoulder protection, and (d) Groin protection.
Figure 5.
Soft body armor: (a) Nomenclature, (b) Neck protection, (c) Shoulder protection, and (d) Groin protection.
Figure 6.
Wave propagation phenomenon in fabric: (a) fabric impacted area and (b) cone formation when hit by a projectile. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier), (c) Piercing in a lightweight composite, (d and e) transverse deflection in fiber. (Reproduced with permission from International Journals of Solids and Structures; Copyright 2003, Elsevier).
Figure 6.
Wave propagation phenomenon in fabric: (a) fabric impacted area and (b) cone formation when hit by a projectile. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier), (c) Piercing in a lightweight composite, (d and e) transverse deflection in fiber. (Reproduced with permission from International Journals of Solids and Structures; Copyright 2003, Elsevier).
Figure 7.
Chemical structure of aramid fiber: (a) meta-aramid and (b) para-aramid [
71]. (Reproduced with permission from Applied Sciences; Copyright 2024, MDPI).
Figure 7.
Chemical structure of aramid fiber: (a) meta-aramid and (b) para-aramid [
71]. (Reproduced with permission from Applied Sciences; Copyright 2024, MDPI).
Figure 8.
Chemical structure of UHMWPE. (Reproduced with permission from Protection from ballistic threats: an exploration of textile materials for bullet-resistant outerwear.; Copyright 2025, Zastita Materijala).
Figure 8.
Chemical structure of UHMWPE. (Reproduced with permission from Protection from ballistic threats: an exploration of textile materials for bullet-resistant outerwear.; Copyright 2025, Zastita Materijala).
Figure 9.
Material property charts: (a) tensile strength against Young’s modulus and (b) specific energy absorption vs velocity of propagation of the longitudinal wave (equation 2.1) of high-performance fibers. Contours of the Cunniff velocity, c*, are also plotted on (b) [
79]. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2014, Elsevier).
Figure 9.
Material property charts: (a) tensile strength against Young’s modulus and (b) specific energy absorption vs velocity of propagation of the longitudinal wave (equation 2.1) of high-performance fibers. Contours of the Cunniff velocity, c*, are also plotted on (b) [
79]. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2014, Elsevier).
Figure 10.
Impact energy absorption response of fabric with different coefficients of friction. (Reproduced with permission from international journal for numerical methods in engineering; Copyright 2005, Elsevier).
Figure 10.
Impact energy absorption response of fabric with different coefficients of friction. (Reproduced with permission from international journal for numerical methods in engineering; Copyright 2005, Elsevier).
Figure 11.
Influence of coefficient of friction of fabric on failure mechanism for round (a) and flat nose (b) projectile: (a) µ=1e-7, (b) µ=0.05, (c) µ=0.1, (d) µ=0.19, (e) µ=0.4, and (f) µ=0.6 (Reproduced with permission from composite structure; Copyright 2015, Elsevier).
Figure 11.
Influence of coefficient of friction of fabric on failure mechanism for round (a) and flat nose (b) projectile: (a) µ=1e-7, (b) µ=0.05, (c) µ=0.1, (d) µ=0.19, (e) µ=0.4, and (f) µ=0.6 (Reproduced with permission from composite structure; Copyright 2015, Elsevier).
Figure 12.
Bottom view of ruptured fabric: (a) Plain woven, (b) Basket woven, (c) Knitted fabric, along with experimental data for (d) Woven and (e) Knitted fabrics. (Reproduced with permission from International Journal of Damage Mechanics; Copyright 2014, SAGE).
Figure 12.
Bottom view of ruptured fabric: (a) Plain woven, (b) Basket woven, (c) Knitted fabric, along with experimental data for (d) Woven and (e) Knitted fabrics. (Reproduced with permission from International Journal of Damage Mechanics; Copyright 2014, SAGE).
Figure 13.
Different stitched fabric systems: (a) 1-inch diamond, (b) 2-inch diamond, (c) Diagonal, and (d) Perimeter. (Reproduced with permission from Materials and design; Copyright 2008, Elsevier).
Figure 13.
Different stitched fabric systems: (a) 1-inch diamond, (b) 2-inch diamond, (c) Diagonal, and (d) Perimeter. (Reproduced with permission from Materials and design; Copyright 2008, Elsevier).
Figure 14.
Different fabric sequences are used in the FEA simulation. (Reproduced with permission from Composite Part B; Copyright 2015, Elsevier).
Figure 14.
Different fabric sequences are used in the FEA simulation. (Reproduced with permission from Composite Part B; Copyright 2015, Elsevier).
Figure 15.
Basic 2D woven fabric configurations: (a) plain, (b) basket, (c) twill. (Reproduced with permission from Wearable Electronics and Photonics; Copyright 2005, Book Chapter).
Figure 15.
Basic 2D woven fabric configurations: (a) plain, (b) basket, (c) twill. (Reproduced with permission from Wearable Electronics and Photonics; Copyright 2005, Book Chapter).
Figure 16.
Different 2D knitted fabric configurations. (Reproduced with permission from Textile Fibre Composites in Civil Engineering; Copyright 2016, Elsevier).
Figure 16.
Different 2D knitted fabric configurations. (Reproduced with permission from Textile Fibre Composites in Civil Engineering; Copyright 2016, Elsevier).
Figure 17.
Schematics of actual 3D woven fabric. (Reproduced with permission from Oxford Open Materials Science; Copyright 2023, Oxford University Press).
Figure 17.
Schematics of actual 3D woven fabric. (Reproduced with permission from Oxford Open Materials Science; Copyright 2023, Oxford University Press).
Figure 18.
Schematics of non-interlaced 3D fabric structures. (Reproduced with permission from Oxford Open Materials Science; Copyright 2023, Oxford University Press).
Figure 18.
Schematics of non-interlaced 3D fabric structures. (Reproduced with permission from Oxford Open Materials Science; Copyright 2023, Oxford University Press).
Figure 19.
Different projectile geometries used for perforation resistance of fabric. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier). Front view of the conical projectiles with varying nose angles. (Reproduced with permission from composite structure; Copyright 2009, Elsevier). Curves of (c) impact load vs time, (d) residual velocity vs time at strike velocity of 176 m/s. (Reproduced with permission from Defence Technology; Copyright 2023, Elsevier).
Figure 19.
Different projectile geometries used for perforation resistance of fabric. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier). Front view of the conical projectiles with varying nose angles. (Reproduced with permission from composite structure; Copyright 2009, Elsevier). Curves of (c) impact load vs time, (d) residual velocity vs time at strike velocity of 176 m/s. (Reproduced with permission from Defence Technology; Copyright 2023, Elsevier).
Figure 20.
Damage progression in the laminate subjected to impact: (a) Conical projectile and (b) Blunt projectiles at different angles (0˚, 15˚, 30˚, and 45˚) of incidence. (Reproduced with permission from Defence Technology; Copyright 2023, Elsevier).
Figure 20.
Damage progression in the laminate subjected to impact: (a) Conical projectile and (b) Blunt projectiles at different angles (0˚, 15˚, 30˚, and 45˚) of incidence. (Reproduced with permission from Defence Technology; Copyright 2023, Elsevier).
Figure 21.
Stab resistance test: (a) Test setup and (b) Backing materials. (Reproduced with permission from Thin-Walled Structures; Copyright 2021, Elsevier).
Figure 21.
Stab resistance test: (a) Test setup and (b) Backing materials. (Reproduced with permission from Thin-Walled Structures; Copyright 2021, Elsevier).
Figure 22.
Single yarn pull-out sample: (a) Schematic of the sample and (b) Pull-out force vs displacement plot. (Reproduced with permission from Thin-Walled Structures; Copyright 2020, Elsevier).
Figure 22.
Single yarn pull-out sample: (a) Schematic of the sample and (b) Pull-out force vs displacement plot. (Reproduced with permission from Thin-Walled Structures; Copyright 2020, Elsevier).
Figure 23.
The quasi-static puncture test: (a) Fabric subjected to the puncture test and (b) Force vs displacement curve. (Reproduced with permission from Composite Part-B; Copyright 2020, Elsevier).
Figure 23.
The quasi-static puncture test: (a) Fabric subjected to the puncture test and (b) Force vs displacement curve. (Reproduced with permission from Composite Part-B; Copyright 2020, Elsevier).
Figure 24.
Penetration depth: (a) Knife and (b) Spike on the backing for different targets. (Reproduced with permission from Thin-Walled Structures; Copyright 2021, Elsevier).
Figure 24.
Penetration depth: (a) Knife and (b) Spike on the backing for different targets. (Reproduced with permission from Thin-Walled Structures; Copyright 2021, Elsevier).
Figure 25.
Schematic setup for ballistic test (NIJ Standard 0101.06). (Reproduced from Ballistic Resistance of Body Armor NIJ Standard-0101.06).
Figure 25.
Schematic setup for ballistic test (NIJ Standard 0101.06). (Reproduced from Ballistic Resistance of Body Armor NIJ Standard-0101.06).
Figure 26.
Varying sizes of targets and clamping patterns: (a) 4- side clamping, (b) Circular clamping, (c) Diamond clamping, and (d) V50 vs fabric exposed area. (Reproduced with permission from composite structure; Copyright 2014, Elsevier).
Figure 26.
Varying sizes of targets and clamping patterns: (a) 4- side clamping, (b) Circular clamping, (c) Diamond clamping, and (d) V50 vs fabric exposed area. (Reproduced with permission from composite structure; Copyright 2014, Elsevier).
Figure 27.
Change in obliquity: (a) By changing the firing line and (b) Changing the angle of the impact surface. (Reproduced with permission from composite structure; Copyright 2019, Elsevier).
Figure 27.
Change in obliquity: (a) By changing the firing line and (b) Changing the angle of the impact surface. (Reproduced with permission from composite structure; Copyright 2019, Elsevier).
Figure 28.
Sample preparation for yarn extraction: (a) Single yarn and (b) Multi-yarn, and load-displacement curve of (c) Neat fabric, (d) stick-slip region in neat fabric, (e) 70 wt% STF-impregnated fabric, and (f) Stick-slip region for STF-impregnated fabric. (Reproduced with permission from Composite Part A; Copyright 2017, Elsevier), (Reproduced with permission from composite structure; Copyright 2013, Elsevier), and (Reproduced with permission from Composite Part B; Copyright 2019, Elsevier).
Figure 28.
Sample preparation for yarn extraction: (a) Single yarn and (b) Multi-yarn, and load-displacement curve of (c) Neat fabric, (d) stick-slip region in neat fabric, (e) 70 wt% STF-impregnated fabric, and (f) Stick-slip region for STF-impregnated fabric. (Reproduced with permission from Composite Part A; Copyright 2017, Elsevier), (Reproduced with permission from composite structure; Copyright 2013, Elsevier), and (Reproduced with permission from Composite Part B; Copyright 2019, Elsevier).
Figure 29.
SEM pictograph of fibrillation: (a) Aramid fibers at 100 µm and Twaron fibers impacted, (b) SEM images (500x) of ruptured fibers (virgin aramid) and (c) Fibrillation in failure region. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier) and (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier).
Figure 29.
SEM pictograph of fibrillation: (a) Aramid fibers at 100 µm and Twaron fibers impacted, (b) SEM images (500x) of ruptured fibers (virgin aramid) and (c) Fibrillation in failure region. (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier) and (Reproduced with permission from International Journal of Impact Engineering; Copyright 2003, Elsevier).
Figure 30.
Pyramid formation in fabric under impact load. (Reproduced with permission from Composite Part B; Copyright 2003, Elsevier).
Figure 30.
Pyramid formation in fabric under impact load. (Reproduced with permission from Composite Part B; Copyright 2003, Elsevier).
Figure 31.
Formation of a pyramid: (a) Visualisation of a high-speed camera and (b) Schematization. (Reproduced with permission from composite structure; Copyright 2013, Elsevier).
Figure 31.
Formation of a pyramid: (a) Visualisation of a high-speed camera and (b) Schematization. (Reproduced with permission from composite structure; Copyright 2013, Elsevier).
Figure 32.
The bowing of yarn: (a) 2D plain weave and (b) 3D warp interlock panel fabric. (Reproduced with permission from Journal of Industrial Textiles; Copyright 2019, SAGE).
Figure 32.
The bowing of yarn: (a) 2D plain weave and (b) 3D warp interlock panel fabric. (Reproduced with permission from Journal of Industrial Textiles; Copyright 2019, SAGE).
Figure 33.
Puncture resistance test: (a) Test setup and (b) Force vs displacement curve for different rubber-coated fabrics. (Reproduced with permission from composite structure; Copyright 2015, Elsevier).
Figure 33.
Puncture resistance test: (a) Test setup and (b) Force vs displacement curve for different rubber-coated fabrics. (Reproduced with permission from composite structure; Copyright 2015, Elsevier).
Figure 34.
The schematic of jute rubber composites arranged in different stacking sequences. (Reproduced with permission from composite structure; Copyright 2019, Elsevier).
Figure 34.
The schematic of jute rubber composites arranged in different stacking sequences. (Reproduced with permission from composite structure; Copyright 2019, Elsevier).
Figure 35.
Steady rheology data of PMMA-based STF at varying ϕ. (Reproduced with permission from Proceedings of the International SAMPE Symposium and Exhibition.; Copyright 2007).
Figure 35.
Steady rheology data of PMMA-based STF at varying ϕ. (Reproduced with permission from Proceedings of the International SAMPE Symposium and Exhibition.; Copyright 2007).
Figure 36.
Effect of particle shapes on the viscosity of the suspension. (Reproduced with permission from Journal of Materials Research and Technology; Copyright 2020, Elsevier).
Figure 36.
Effect of particle shapes on the viscosity of the suspension. (Reproduced with permission from Journal of Materials Research and Technology; Copyright 2020, Elsevier).
Figure 37.
Rheology of silica colloidal suspension: (a) viscosity vs shear rate for different particle sizes, (b) CSR vs particle size curve. (Reproduced with permission from Journal of Composite Materials; Copyright 2009, Elsevier).
Figure 37.
Rheology of silica colloidal suspension: (a) viscosity vs shear rate for different particle sizes, (b) CSR vs particle size curve. (Reproduced with permission from Journal of Composite Materials; Copyright 2009, Elsevier).
Figure 38.
Effect of particle roughness on suspension rheology. (Reproduced with permission from Physical Review Letters; Copyright 2017, AIP Publishing).
Figure 38.
Effect of particle roughness on suspension rheology. (Reproduced with permission from Physical Review Letters; Copyright 2017, AIP Publishing).
Figure 39.
Rheological behavior of STF under varying temperatures: (a) PEG 200-STF, (b) PEG 400-STF, (c) 1,3-propandiol-STF, (d) Glycerine-STF. (Reproduced with permission from composite structure; Copyright 2020, Elsevier).
Figure 39.
Rheological behavior of STF under varying temperatures: (a) PEG 200-STF, (b) PEG 400-STF, (c) 1,3-propandiol-STF, (d) Glycerine-STF. (Reproduced with permission from composite structure; Copyright 2020, Elsevier).
Figure 40.
Rheological behavior of multiphase STFs: (a) Viscosity vs shear rate and (b) Thickening period and ratio for different STFs. (Reproduced with permission from Thin-walled Structures; Copyright 2020, Elsevier).
Figure 40.
Rheological behavior of multiphase STFs: (a) Viscosity vs shear rate and (b) Thickening period and ratio for different STFs. (Reproduced with permission from Thin-walled Structures; Copyright 2020, Elsevier).
Table 1.
Properties of glass fibers.
Table 1.
Properties of glass fibers.
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3
|
GPa |
MPa |
% |
| E-glass |
2.58 |
72 |
2600 |
3.0 |
| S- glass |
2.48 |
90 |
4400 |
5.7 |
Table 2.
Properties of carbon fibers (PAN).
Table 2.
Properties of carbon fibers (PAN).
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3 |
GPa |
MPa |
% |
| Celion |
1.80 |
230 |
4000 |
1.8 |
| Aksaca |
1.78 |
240 |
4200 |
1.8 |
Table 3.
Properties of ceramic fibers.
Table 3.
Properties of ceramic fibers.
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3 |
GPa |
MPa |
% |
| Alumina |
2.50 |
152 |
1720 |
2.0 |
| Silicon carbide |
2.80 |
420 |
4000 |
0.6 |
Table 4.
Properties of aramid fibers [
69,
71].
Table 4.
Properties of aramid fibers [
69,
71].
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3
|
GPa |
MPa |
% |
| Kevlar 29 |
1.44 |
70 |
3300 |
4.2 |
| Kevlar 49 |
1.45 |
135 |
3300 |
2.8 |
| Kevlar 129 |
1.45 |
99 |
3400 |
3.3 |
| Kevlar 149 |
1.47 |
143 |
3600 |
1.5 |
| Twaron |
1.45 |
121 |
3100 |
2.0 |
Table 5.
Properties of UHMWPE fibers.
Table 5.
Properties of UHMWPE fibers.
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3
|
GPa |
MPa |
% |
| Spectra 900 |
0.97 |
73 |
2400 |
2.8 |
| Spectra 1000 |
0.97 |
103 |
2830 |
2.8 |
| Spectra 2000 |
0.97 |
124 |
3340 |
3.0 |
| Dyneema |
0.97 |
87 |
2600 |
3.5 |
| Zylon |
1.56 |
270 |
5800 |
2.5 |
Table 6.
Properties of Zylon fibers.
Table 6.
Properties of Zylon fibers.
| Fiber type |
Density |
Tensile modulus |
Tensile strength |
Fracture strain |
| |
g/cm3 |
GPa |
MPa |
% |
| Zylon |
1.56 |
270 |
5800 |
2.5 |
Table 7.
Evolution in the nomenclature of 3D fabric.
Table 7.
Evolution in the nomenclature of 3D fabric.
| S.N. |
Former name |
Updated name |
| 1 |
Orthogonal 3D woven fabric |
Orthogonal interlock, through-thickness |
| 2 |
3D Warp interlock |
Orthogonal interlock, layer-to-layer |
| Angle interlock, layer-to-layer |
| 3 |
3D Angle interlock |
Angle interlock, through-thickness |
Table 8.
HOSDB ballistic resistance protection levels.
Table 8.
HOSDB ballistic resistance protection levels.
| Protection level |
Description |
| HG1/A |
This is the lowest ballistic protection level for HOSDB, and the BFS can be up to 44 mm and cannot exceed this.
|
| HG1 |
This is recommended for use in low-risk areas and can be operated overtly and covertly.
|
| HG2 |
Recommended for special operations where the chance of shootings is high.
|
| HG3 |
Suggested for heavy-duty body armor and generally employed with RF and SG hard armor plates. |
| SG1 |
Provides protection against shotguns at close range. |
| RF1 |
Ensures defense against soft-core ammunition from rifles. |
| RF2 |
Safeguards against steel core ammunition from rifles and the maximum protection for hard armor panels. |
Table 9.
Stab-resistant protection level strike energies.
Table 9.
Stab-resistant protection level strike energies.
| Protection level |
Energy level |
Strike Energy (J) |
Overtest Energy (J) |
| Level-1 |
Low |
24 |
36 |
| Level-2 |
Medium |
33 |
50 |
| Level-3 |
High |
43 |
65 |