NANA Twitter header ꩜ .ᐟ Nana Komatsu / Hachi theme ( free use , made by kanekamedia )

Completed in 2021 in Takasago, Japan. Images by Norihito Yamauchi. KANEKA Wellness Center is Kaneka Corporation’s welfare facility, which also functions as a medical facility. With its corporate policy including...

上質な家具・ソファを販売する京都の家具・インテリアショップ「KANEKA（カネカ家具）」。 無垢材を使ったオーダーメイド家具・ソファを中心に最大10年保証付き。

Image 1 of 29 from gallery of KANEKA Wellness Center / Kengo Kuma & Associates + TAISEI DESIGN Planners Architects & Engineers. Photograph by Norihito Yamauchi

給湯及び温水暖房端末用リモコン。台所や浴室に設置し機器の操作を行う。スタイリッシュなデザインで高級から普及ゾーンまでを網羅する。デザインはシンプルで直線を基調にしインテリアの中で必要以上に主張をしない様にまとめた。高級タイプはドットマトリクスを使用し、より細かなエネルギー情報の表示や複数の温水暖房端末の操作が可能。普及タイプは表示する情報量を減らしキャラクター表示にし見易くした。操作スイッチは日常良く使用する給湯関係の操作スイッチを表に出し、副操作スイッチは蓋の中に入れスッキリさせた。停電をしても自動車のソケットに繋げば、応急的にお湯が仕様可能な「停電モード」を搭載。

金具を一切使わず、木の細工だけで伸長させる、画期的な天然木無垢材ダイニングテーブル「クラシック」をご紹介します

Japanese designer Michiru Tanaka has released a new product partnering with lighting manufacturer Kaneka to create a stainless steel tile that...

transforming the superstudio piu, milan into a foggy, soft-lit atmosphere, designer chikara ohno of sinato has designed 'infuse' for kaneka corporation.

These seamlessly integrated lighting solutions by Philips, Fluvia Meystyle and Kaneka OLED transform walls into art. Explore a lighting installation, LED wall tiles, illuminated wallpaper and more.

Gluten Free Non GMO LE CertifiedEnhanced Delivery System for Maximum AbsorptionDietary SupplementMade with Quality Q+®, Kaneka Ubiquinol™CoQ10 offers lots of heart-healthy benefits, but standard CoQ10 (called ubiquinone) is not well absorbed by the body. Ubiquinol CoQ10 maintains healthy blood concentrations better than standard CoQ10, meaning it is more bioavailable—and this customer-favorite formula is

Description FABRICS WITH BALLISTIC PROTECTION AND GARMENTS MADE FROM SAME FIELD Embodiments of the present invention relate to fabrics that provide ballistic protection as well as garments made from such fabrics. BACKGROUND In combat environments, much attention is focused on preventing injuries caused by relatively large projectiles and fragmentation, such as those emanating from improvised explosive devices. However, significant damage can also be caused by ejecta (small particles of sand and other fine grain projectiles typically moving between 500-1200 ft./sec.) that penetrate through garments and harm underlying skin and tissue. If left in skin and tissue, the ejecta can cause infection which can ultimately lead to amputation of the affected area. While a number of ballistic fabrics have been developed and provide protection, none do so while still being comfortable to the wearer and dyeable/ printable. Thus, there is a need to provide fabrics that afford protection against ejecta while being comfortable to the wearer and dyeable/ printable. The ability of a fabric to protect against ejecta is measured pursuant to the testing methodology set forth in MIL-STD-662F, Department of Defense Test Method Standard, V50 Ballistic Test for Armor, December 18, 1997. The required performance of a fabric tested pursuant to this methodology is dependent on the garment in which the fabric is to be used. SUMMARY The terms "invention," "the invention," "this invention" and "the present invention" used in this patent are intended to refer broadly to all of the subject matter of this patent and the patent claims below. Statements containing these terms should not be understood to limit the subject matter described herein or to limit the meaning or scope of the patent claims below. Embodiments of the invention covered by this patent are defined by the claims below, not this summary. This summary is a high-level overview of various aspects of the invention and introduces some of the concepts that are further described in the Detailed Description section below. This summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used in isolation to determine the scope of the claimed subject matter. The subject matter should be understood by reference to the entire specification of this patent, all drawings and each claim. Certain embodiments of the present invention provide fabrics having fiber blends and constructions engineered to enhance the ballistic protection of such fabrics (or the garments into which the fabrics are made or otherwise incorporated) while also enhancing the comfort and/ or dyeability/ printability of such fabrics. DETAILED DESCRIPTION Fabrics according to embodiments of this invention have fibers and constructions that enhance the ballistic protection of the fabric. Fabrics according to some embodiments of this invention may also be, but do not have to be, flame resistant. For example, the fabrics may comply with the thermal protective requirements set forth in NFPA 2112 (2007), including having acceptable char lengths (as measured with the testing method set forth in ASTM D6413), as well as GL-PD-07-12 Rev. 5 (Sept. 28, 2012) and GL-PD-10-02C (Sept. 1, 2010), the entirety of which are hereby incorporated by reference. In some embodiments, the fabric includes fibers that enhance the ballistic protection of the fabric (referred to as "ballistic fibers"). The ballistic fibers may be stretch broken ballistic fibers, staple ballistic fibers (including long and short staple), and/ or filament ballistic fibers, or a combination of such fibers. The ballistic fibers used in some embodiments of the fabrics contemplated herein include, but are not limited to, para-aramid fibers, ultra-high density polyethylene fibers, polybenzoxazole (PBO) fibers, carbon fibers, silk fibers, polyamide fibers, polyester fibers, and poly{2,6- diimidazo[4,5-b:40; 50-e]-pyridinylene-l,4(2,5-dihydroxy)phenylene} ("PIPD") fibers. Examples of para-aramid fibers include KEVLAR™ (available from DuPont), TECHNORA™ (available from Teijin Twaron BV of Arnheim, Netherlands), and TWARON™ (also available from Teijin Twaron BV). Examples of ultra-high density polyethylene fibers include Dyneema and Spectra. An example of a polyester fiber is VECTRAN™ (available from Kuraray). An example of a PIPD fiber includes M5 (available from Dupont). In some embodiments, the fabrics are formed from 100% ballistic fibers. For example, all of the yarns in the fabric may be formed with 100% of a single type of ballistic fiber or alternatively a blend of different ballistic fibers. Moreover, yarns formed from 100% ballistic fibers may be all or an intimate blend of staple fibers, a combination of filament fibers, or a combination of filament fibers and staple fibers. In other embodiments, the fabric includes ballistic fibers (such as those disclosed above) and one or more types of secondary fibers that are used to enhance a secondary property of the fabric other than ballistic protection (e.g., comfort, dyeability/printability, etc.) (referred to as "secondary fibers"). The secondary fibers can be staple or filament fibers and can be flame resistant or used in their non-flame resistant state (to the extent possible). For example, some embodiments of the fabric may be formed from yarns having 100% ballistic fibers (such as those disclosed above) and yarns that include one or more types of secondary fibers (either in addition to, or to the exclusion of, ballistic fibers). In other embodiments, yarns forming the fabric are formed from a blend of one or more ballistic fibers (such as those disclosed above) and one or more types of secondary fibers. The blended yarns may be a combination of spun fibers, a combination of filament fibers, or a combination of filament fibers and staple fibers. Such secondary fibers can be selected to enhance a property of the fabric, such as, but not limited to, the comfort, durability, and/ or dyeability/ printability of the fabric. Secondary fibers that enhance the comfort of the fabric (i.e., have higher moisture regain, soft hand, etc.) are referred to herein as "comfort fibers." "Comfort fibers" as used herein include, but are not limited to, cellulosic fibers, polybenzimidazole (PBI) fibers, TANLON™ (available from Shanghai Tanlon Fiber Company), rayon, wool, and blends thereof. Examples of cellulosic fibers include cotton, rayon, acetate, triacetate, MODAL™, and lyocell fibers (as well as their flame resistant counterparts FR cotton, FR rayon, FR acetate, FR triacetate, and FR lyocell). An example of a suitable rayon fiber is Viscose by Lenzing, available from Lenzing Fibers Corporation. Examples of lyocell fibers include TENCEL G100™ and TENCEL A100™, both available from Lenzing Fibers Corporation. Examples of FR rayon fibers include Lenzing FR™ and Lenzing RF™, also available from Lenzing Fibers Corporation, and VISIL™, available from Sateri. Secondary fibers that enhance the dyeability/printability of the fabric are referred to herein as "dyeable fibers" and include fibers that are dyeable and dyestuff printable (as opposed to pigment printable). "Dyeable fibers" as used herein include, but are not limited to, modacrylic fibers, cellulosic fibers, meta-aramid fibers, polybenzimidazole (PBI) fibers, melamine fibers, TANLON™ (available from Shanghai Tanlon Fiber Company), rayon, polyester, polyvinyl alcohol, wool, polyetherimide, polyethersulfone, polyamide, and blends thereof. An example of suitable modacrylic fibers are PROTEX™ fibers available from Kaneka Corporation of Osaka, Japan, SEF™ available from Solutia, or blends thereof. Examples of cellulosic fibers include cotton, rayon, acetate, triacetate, MODAL™, and lyocell fibers (as well as their flame resistant counterparts FR cotton, FR rayon, FR acetate, FR triacetate, and FR lyocell). An example of a suitable rayon fiber is Modal by Lenzing, available from Lenzing Fibers Corporation. Examples of lyocell fibers include TENCEL G100™ and TENCEL A100™, both available from Lenzing Fibers Corporation. Examples of FR rayon fibers include Lenzing FR™ and Lenzing RF™, also available from Lenzing Fibers Corporation, and VISIL™, available from Sateri. Examples of meta-aramid fibers include NOMEX™ (available from DuPont), CONEX™ (available from Teijin), and Kermel (available from Kermel). An example of melamine fibers is BASOFIL™ (available from Basofil Fibers). In some embodiments, the ballistic fibers comprise 25-100% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 0-75% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 25-80% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 20-75% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 45-70% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 30-55% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 40-60% and the secondary fibers comprise 40-60% of the fibers in the fabric. It may be, but will not always be, the case that, to the extent a smaller percentage of ballistic fibers are used in the fabric, the fabric weight may need to be increased to achieve the desired ballistic protection. The fabric may also include fibers in addition to the ballistic and secondary fibers identified above. For example, some fabric embodiments may also include fibers that enhance static dissipation of the fabric (referred to herein as "antistat fibers"). Examples of antistat fibers can include, but are not limited to, fibers having a carbon core surrounded by a nylon or polyester sheath. An example of an antistat fiber includes No-Shock® (available from Ascend Performance Materials), and an example of an antistat filament yarn includes Mega-Stat® (available from Barnet). The yarns in the fabric may be spun or filament yarns and can comprise a single yarn or two or more individual yarns that are combined together in some form, including, but not limited to, twisting, plying, tacking, wrapping, covering, core- spinning (i.e., a filament or spun core at least partially surrounded by spun fibers or yarns), etc. In some embodiments, the fabrics can be formed entirely from yarns having identical fiber blends (i.e., all of the yarns in the fabric are the same) such that the fabrics have the overall blends of ballistic and secondary fibers set forth above. Where identical yarns are used, the fabrics may be formed by traditional weaving technology and traditional knitting technology (e.g., warp knits with various styles and constructions (such as raschel, tricot, and simplex) and weft knits with various styles and constructions (such as flat bed and circular knits, such as double knits (including swiss pique, rib, interlock, etc.) and single knits (including jersey and pique))). However, in other embodiments, the yarns forming the fabric may not all be identical. For example, it may be desirable to form the fabric from a first type of yarn engineered more for ballistic protection (hereinafter referred to as the "ballistic yarns") and a second type of yarn engineered more for a secondary property, such as comfort and/ or dyeability/ printability (hereinafter referred to as the "secondary yarns"). Use of the terms "ballistic yarns" and "secondary yarns" is not meant to suggest that the ballistic yarns do not or cannot impart comfort and/ or dyeability/ printability or that the secondary yarns do not or cannot impart any ballistic protection. The ballistic yarns may include a higher percentage of ballistic fibers than the secondary yarns to impart ballistic protection to the fabric, and the secondary yarns may include a higher percentage of secondary fibers (comfort fibers or dyeable fibers) to impart comfort and dyeability/ printability, respectively, to the fabric. However, such may not always be the case. The ballistic yarns may be formed of one type of ballistic fiber or formed from a combination of fibers (ballistic fibers, secondary fibers, antistat fibers, or other types of fibers). The ballistic yarns may be spun or filament yarns and can comprise a single yarn or two or more individual yarns that are combined together in some form, including, but not limited to, twisting, plying, tacking, wrapping, covering, core- spinning (i.e., a filament or spun core at least partially surrounded by spun fibers or yarns), etc. In some embodiments, the ballistic yarns are formed with 100% ballistic filament yarns. In some embodiments, the ballistic yarns include 100% para-aramid filament yarns. In other embodiments, the ballistic yarns include 100% high density polyethylene filament yarns. The ballistic yarns may also be spun yarns. In one such non-limiting embodiment, the ballistic yarns are formed of a blend of 80-100% para-aramid fibers and 0-20% cellulosic fibers. In another embodiment, the ballistic yarns are formed of a blend of 50-80% para-aramid fibers and 20-50% cellulosic fibers. Additional fiber types (including, but not limited to, other of the ballistic fibers, comfort fibers, dyeable fibers, antistat fibers, etc.) may also be included in such blends. The secondary yarns may be formed of one type of secondary fiber or formed from a combination of fibers (ballistic fibers, secondary fibers, antistat fibers, or other types of fibers). In some embodiments, the secondary yarns include a combination of fibers. The secondary yarns may be spun or filament yarns and can comprise a single yarn or two or more individual yarns that are combined together in some form, including, but not limited to, twisting, plying, tacking, wrapping, covering, core- spinning (i.e., a filament or spun core at least partially surrounded by spun fibers or yarns), etc. Exemplary but non-limiting combinations of secondary yarns include, but are not limited to: (i) 20-100% cellulosic fibers and 0-80% para-aramid fibers; (ii) 20-50% cellulosic fibers and 50-80% para-aramid fibers; (iii) 30-50% cellulosic fibers, 30-50% modacrylic fibers, and 0-40% para-aramid fibers; (iv) 20-100% meta-aramid fibers and 0- 80% cellulosic fibers; (v) 20-100% nylon fibers and 0-80% cellulosic fibers; and (vi) 20- 100% modacrylic fibers and 0-80% cellulosic fibers. Such blends may be tailored depending on the desired secondary property of the fabric (comfort, dyeability/ printability, etc.). Moreover, such blends may also include other fibers types (including, but not limited to, other of the ballistic fibers, comfort fibers, and/ or dyeable fibers identified above). The ballistic yarns may be combined with secondary yarns in various ways to form various fabric embodiments. Yarns formed of differing fiber blends (e.g., ballistic and secondary yarns) may be woven or knitted in different ways, some of which result in different properties being imparted to different sides of the fabric. For example and with respect to weaving, one of the warp or fill yarns could be of the ballistic yarns and the other of the warp or fill yarns could be of the secondary yarns. The fabric could be woven (such as via a twill or Satin weave construction) so that the warp and fill yarns (and thus the ballistic and secondary yarns) are exposed predominantly on opposing sides of the fabric. In this way, one side of the fabric contributes more ballistic protection while the other side of the fabric contributes more of the desired secondary property (comfort, dyeability/printability, etc., depending on the make-up of the secondary yarns). In other embodiments, not all of the warp or fill yarns are the same. For example, ballistic and secondary yarns may be provided in both the warp and fill directions by providing ballistic yarns on some ends and picks and secondary yarns on other ends and picks (in any sort of random arrangement or alternating pattern). Or all of the yarns in one of the warp or fill direction could be identical and different yarns used only in the other of the warp or fill direction. Similarly and with respect to knitting, ballistic yarns may be knitted with secondary yarns in a variety of ways. The ballistic and secondary yarns may be knitted using single knit technology (e.g., plating) or double-knit technology such that the ballistic yarns will be located primarily on one side of the fabric to enhance ballistic protection and the secondary yarns will be located primarily on the opposing side of the fabric to enhance comfort or dyeability/printability (or whatever secondary property the secondary yarn is tailored to have) to the fabric. In yet another embodiment, the ballistic and secondary yarns are knitted so that alternating courses and/ or wales of the fabric are formed by different yarn types. In still yet another embodiment, the fabric may be knitted (such as using double-knit plating technology) such that one of the ballistic and secondary yarns is embedded within the fabric so as not to be exposed on a fabric surface and the other of the ballistic and secondary yarns is exposed on both sides of the fabric. In some embodiments, the ballistic yarn is embedded in the fabric to enhance the ballistic protection of the fabric while leaving the secondary yarns exposed on the fabric surface to enhance the comfort or dyeablity/ printability to the fabric. Fabrics formed of ballistic and secondary yarns provided on opposing sides of the fabric may be oriented in a variety of ways within a garment, depending on the use of the garment. For example, if incorporated into garments where it is desirable that the exterior of the garment be dyed or printed (e.g., camouflage), it may useful to incorporate secondary yarns into the fabric and expose the side of the fabric with the secondary yarns (which will typically be more conducive to dyeing and/ or printing) on the exterior of the garment and the ballistic yarns facing the wearer. Alternatively, if dyeing or printing of the fabric is of no consequence, it may be desirable to incorporate secondary yarns into the fabric and position the side of the fabric with the secondary yarns (which will typically be more comfortable) in the garment so that the comfort yarns are facing the wearer. In some embodiments, it may be desirable, but certainly not required, to incorporate stretchable yarns ("stretch yarns") into the fabrics, which may improve the ballistic protection of the fabrics. Stretch yarns may be yarns formed from inherently elastic materials such as spandex (elastane), ethylene-olefin copolymer, rubber or similar elastomeric-type materials or alternatively could be formed from non- inherently stretchable yarns (e.g., nylon yarns, polyester yarns, etc.) that have been chemically or physically altered (such as via crimping, texturing, etc.) to render them elastic or stretchable. Examples of spandex fibers include LYCRA™ (available from Invista), DORLASTAN™ (available from AsahiKasei Spandex America), and RadiciSpandex. Examples of ethylene-olefin copolymer fibers include Dow XLA™ composite fibers. In some embodiments, the stretch yarns are filament yarns formed from the elastomeric fibers disclosed above. The stretch yarns are not particularly durable or resistant to heat and fire and thus tend to degrade or melt from exposure to such extreme conditions. Thus, it may be desirable, but certainly not required, to orient other yarns or fibers that do have some heat/ flame resistance at least partially around the stretch yarns so as to protect them. The flame resistant yarns (which may include the ballistic and/ or secondary yarns disclosed above) may be oriented at least partially around the stretch yarns, such as via plying or helically wrapping the stretch yarns. U.S. Patent Nos. 5,527,597 and 5,694,981 (both of which are incorporated herein in their entirety) illustrate fabric configurations whereby stretch yarns are helically wrapped with flame resistant yarns to form a protected stretch yarn (see Figure 1). A single flame resistant yarn or multiple flame resistant yarns may be used to wrap a stretch yarn. In an alternative embodiment, flame resistant fibers may be spun around the stretch yarn so as to form a protective sheath about the stretch yarns. Again, however, it certainly is not required that the stretch yarns be so protected. For woven fabrics, the stretch yarns may be provided in the warp and/ or fill direction or in both directions. For knitted fabrics, the stretch yarns may be incorporated in a variety of ways. In some embodiments, the stretch yarns may be knitted with the other yarns (such as those described above) using standard knitting techniques, including plating. In some embodiments, not all courses or wales include a stretch yarn. By way only of example, stretch yarns may be provided only in alternating courses or wales. In other embodiments, the stretch yarns are "laid in" during the knitting process. In one such non-limiting configuration, the stretch yarns are not technically knitted with the other yarns but rather are inserted during the knitting process and essentially trapped by the knit structure so as to be retained in the fabric. Blends of the ballistic and secondary fibers disclosed herein may also be used to form a nonwoven fabric. In some embodiments, the ballistic fibers comprise 25-100% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 0-75% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 25-80% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 20-75% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 45-70% and the secondary fibers (comfort fibers, dyeable fibers, or some combination of both) comprise 30-55% of the fibers in the fabric. In some embodiments, the ballistic fibers comprise 40-60% and the secondary fibers comprise 40-60% of the fibers in the fabric. In some embodiments, front/back lapping may be used to form the nonwoven fabric such that the nonwoven fabric has a different blend on the face versus the back of the nonwoven fabric. In some embodiments, the nonwoven fabric is formed with multiple layers. The nonwoven fabric may be formed with any number of layers. Moreover, the fiber blend of the various layers can be, but may not be, the same. Moreover, layers having different fiber blends may be oriented within the nonwoven fabric in any order (e.g., ABAB, ABCABC, ABACABAC, etc., where A, B, and C are each a layer utilizing a unique fiber blend). Ballistic fabrics contemplated herein may consist of a single ply of the woven, knitted, or nonwoven fabrics disclosed herein or alternatively may be formed with multiple plies of such fabrics, by means of quilting, laminating, adhering, etc. In some embodiments, the fabrics contemplated herein have a weight greater than 2.5 ounces/yd2 and less than 12.5 ounces/yd2, inclusive. In some embodiments, the fabrics contemplated herein have a weight of between 2.5-11 ounces/yd2, between 5-9 ounces/yd2, and between 5-7 ounces/yd2, inclusive. In some embodiments, the fabrics have a weight of 6 ounces/yd2, 8.5 ounces/yd2, or 11 ounces/yd2. Embodiments of the fabrics may be tested pursuant to the V50 Ballistic Test set forth in MIL-STD-662F, Department of Defense Test Method Standard, V50 Ballistic Test for Armor, December 18, 1997. INCH-POUND MIL-STD-662F 18 December 1997 SUPERSEDING MIL-STD-662E 22 January 1987 DEPARTMENT OF DEFENSE TEST METHOD STANDARD V BALLISTIC TEST FOR ARMOR AMSC N/A FSC 8470 MIL-STD-662F FOREWORD 1 . This standard is approved for use by all Departments and Agencies of the Department of Defense (DoD). 2. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Director, U.S. Army Research Laboratory, Weapons & Materials Research Directorate, ATTN: AMSRL-WM-M, APG, MD 21005-5069 by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. MIL-STD-662F CONTENTS PARAGRAPH PAGE . SCOPE 1.1 Purpose 1.2 Application 1 .3 Limitations 1 . APPLICABLE DOCUMENTS 2.1 General 2.2 Government documents 2.2.1 Specifications, standards, and handbooks 2.2.2 Other Government documents, drawings and publications 2.3 Order of precedence 2 . DEFINITIONS 2.1 Applique armor 2.2 Areal density 3.3 Armor 3.4 Ballistic acceptance test 3.5 Ballistic coefficient 3.6 Ballistic Impact 3.7 Ballistic limit 3.8 Ballistic limit, protection criteria (V50BL(P)) 4.9 Ballistic resistance 4.10 Ceramic composite armor 4.1 1 Chronograph 4.12 Composite armor 4.13 Fair hits (for ceramic composite armor) 4.14 Fair impact 5.15 Fragment simulator 5.16 Initial velocity 5.17 Integral armor 5.18 Lumiline screen 5.19 Muzzle velocity 5.20 Obliquity 5.21 Obliquity angle 5.22 Overmatch 5.23 Parasitic armor 5.24 Penetration, complete (CP) 5 MIL-STD-662F CONTENTS PARAGRAPH P GE 3.25 Penetration, partial (PP) 6 3.26 Petalling 6 3.27 Projectile, fragment simulating 6 3.28 Propellant 6 3.29 Punching 6 3.30 Sabot 6 3.31 Small arms 6 3.32 Small arms ammunition 6 3.33 Spaced armor 6 3.34 Spalling 6 3.35 Striking velocity 6 3.36 Target base line 6 3.37 Terminal ballistics 7 3.38 Test sample 7 3.39 Undermatch 7 3.40 V50 ballistic limit 7 3.41 Witness plate 7 3.42 Yaw 7 4. GENERAL REQUIREMENTS 7 4.1 Projectile 7 4.2 Weapon 7 4.3 Velocity measuring equipment 7 4.3.1 Chronograph 7 4.3.2 Detectors 7 4.3.3 Radar 8 4.4 Propellant 8 4.5 Test sample mount 8 4.6 Test sample 8 5. DETAILED REQUIREMENTS 8 5.1 Test conditions 8 5.2 Equipment setup 8 5.2.1 Triggering devices 8 5.2.2 Witness plate 9 5.3 Ballistic test procedure 9 5.3.1 Warm-up for constant velocity 9 MIL-STD-662F CONTENTS PARAGRAPH PAGE 5.3.2 Yaw 9 5.3.3 First firing 10 5.3.4 Examination of witness plate 10 5.3.5 Subsequent firings 10 5.4 Calculation of the V50BL(P) ballistic limit 10 5.5 Computation of striking velocity 10 5.6 Ballistic test report 1 1 5.7 Acceptance and rejection 12 5.8 Test samples ownership 12 5.9 Retests 12 5.10 Security classification of armor 2 6. NOTES 12 6.1 Intended Use 12 6.2 Subject term (key word) listing 13 6.3 Changes from previous issue 13 TABLE I. Projectile velocities (feet/second) 14 CONCLUDING MATERIAL 17 MIL-STD-662F 1 . SCOPE 1 .1 Purpose. The purpose of this standard is to provide general guidelines for procedures, equipment, physical conditions, and terminology for determining the ballistic resistance of metallic, nonmetallic and composite armor against small arms projectiles. The ballistic test procedure described in this standard determines the V50 ballistic limit of armor. 1 .2 Application. This test method standard is intended for use in ballistic acceptance testing of armor and for the research and development of new armor materials. This ballistic test method is applicable to the following types of armor: a. Body armor. b. Armored seats for aircraft and ground vehicles. c. Crew station armor for military aircraft. d. Internal and external armor for aircraft. e. Transparent armor, such as windows, windshields and vision blocks for aircraft and ground vehicles. f. Bulkhead armor for shipboard use. g. Structural or integral armor for use on ship exteriors. h. Armor for military tactical shelters (AFWAL-TR-82-4163). i. Visors for eye and face protection. j. Armor for potential space applications. k. Armor for light and heavy combat vehicles and structures. 1 .3 Limitations. This standard has the following limitations: a. When specified by the procuring activity, ballistic acceptance of armor may be based upon pass/fail or accept/reject criteria other than the V50 BL(P) ballistic limit method contained herein. b. Military activities or DoD contractors may use in-house ballistic test facilities and equipment not covered by this standard (see MIL-STD-1 161 ). c. This standard does not take precedence over nor supersede armor specification ballistic test procedures. d. Unique requirements for the ballistic testing of specific end-items not covered in this standard should be specified in the contract. MIL-STD-662F 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, and 5 of this standard. This section does not include documents cited in other sections of this standard or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3, 4, and 5 of this standard, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and handbooks. Not applicable. 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation. ARL PROGRAM No.: 0183009 Security Classification Guide for Armor Materials (30 JULY 1993) (Application for copies should be addressed to U.S. Army Research Laboratory, Intelligence and Security Office, ATTN: AMSRL-OP-SC, 2800 Powder Mill Road, Adelphi, MD 20783-1 145. USATECOM TOP 2-2-7I0 Ballistic Tests of Armor Materials ITOP 4-2-805 Projectile Velocity and Time of Flight Measurements (Application for copies should be addressed to the Defense Technical Information Center, 8725 John J. Kingman Road, Ste. 0944, Fort Belvoir, VA 22060-6218.) 2.3 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. DEFINITIONS 3.1 Applique armor. Armor that can be easily installed or removed from a weapon system in kit form without adversely affecting its structural integrity or operation. MIL-STD-662F 3.2 Areal density. A measure of the weight of armor material per unit area, usually expressed in pounds per square foot (1 b/ft2) or kilograms per square meter (kg/m2) of surface area. 3.3 Armor. A shielding material provided for ballistic defeat of projectiles or fragments when inherent shielding is inadequate. 3.4 Ballistic acceptance test. A test performed on lot representative samples to determine whether or not the lot of armor is ballistically acceptable for use in production armor items. 3.5 Ballistic coefficient. A parameter or measure which is used to represent or account for the attenuation of the velocity of a projectile or fragment in transit from the firing mechanism to the target. "Ballistic coefficients" are normally used in approximate formulations to determine average speed or times-of-flight for a projectile. For example, average projectile speed, Vp, can be obtained from: exp ( ocR)-1 where Vo = muzzle velocity R = range oc = ballistic coefficient 3.6 Ballistic impact. Those impacts due to hits on the target by projectiles, fragments or other aerodynamically-affected threat mechanisms. 3.7 Ballistic limit. The minimum velocity at which a particular projectile is expected to consistently, completely penetrate armor of given thickness and physical properties at a specified angle of obliquity. The ballistic limit may also be defined as the maximum velocity at which a particular projectile is expected to consistently fail to penetrate armor of given thickness and physical properties at a specified angle of obliquity. Because of the expense of firing tests and the impossibility of controlling striking velocity precisely, plus the existence of a zone of mixed results in which a projectile may completely penetrate or only partially penetrate under apparently identical conditions, statistical approaches are necessary, based upon limited firings. Certain approaches lead to approximation of the V50 Point, that is, the velocity at which complete penetration and incomplete penetration are equally likely to occur. Other methods attempt to approximate the Vo Point, that is, the maximum velocity at which no complete penetration will occur. MIL-STD-662F Other methods attempt to approximate the V 0o Point, that is, the minimum velocity at which all projectiles will completely penetrate. 3.8 Ballistic limit, protection criteria (VsoBL(P)). The V50BL(P) may be defined as the average of an equal number of highest partial penetration velocities and the lowest complete penetration velocities which occur within a specified velocity spread. The normal up-and-down firing procedure is used. A 0.020 in. (0.51 mm) thick 2024 T3 sheet of aluminum is placed 6 + 1/2 in. (152 + 12.7 mm) behind and parallel to the target to witness complete penetrations. Normally, at least two partial and two complete penetration velocities are used to complete the BL(P). Four, six, and ten-round ballistic limits are frequently used. The maximum allowable velocity span is dependent on the armor material and test conditions. Maximum velocity spans of 60, 90, 100 and 125 feet per second (ft s) (18, 27, 30 and 38 m/s) are frequently used. 3.9 Ballistic resistance. A measure of the capability of a material or component to stop or reduce the impact velocity and mass of an impacting projectile or fragment. 3.10 Ceramic composite armor. A type of composite armor which consists of a ceramic face bonded to a reinforced plastic laminate or metallic backplate. 3.1 1 Chronograph. An electronic instrument used to determine the time interval of projectile flight between two fixed measuring stations. 3.12 Composite armor. An armor system consisting of two or more different armor materials bonded together to form a protective unit. 3.13 Fair hits (for ceramic composite armor). The definitions contained herein apply to the ballistic testing of ceramic composite armor which consists (in part) of ceramic tiles. a. Fair hit (center tile) - A fair hit for the center tile of the ceramic composite armor is an area within one inch (25.4 mm) radius of the center of an undamaged tile. b. Fair hit (adjacent tile) - A fair hit in an adjacent tile is a fair hit (center tile) in a tile that has an edge adjacent to a previously impacted tile whose hit was declared a fair hit. c. Fair hit (joint line) - A fair hit on a joint line is a hit within 0.15 in. (3.8 mm) of a single joint between two tiles, but no closer than 0.5 in. (12.7 mm) from the intersection of three or more tiles. MIL-STD-662F 3.14 Fair impact. An impact shall be considered fair when an unyawed (see 5.3.2) fragment simulator or test projectile strikes an unsupported area of the target material at a specified obliquity at a distance of at least two projectile diameters from any previous impact or disturbed area resulting from an impact, or from any crack, or from any edge of the test specimen. 3.15 Fragment simulator. A projectile designed to simulate the effects of fragmenting munitions when such fragments strike a target. 3.16 Initial velocity. The projectile velocity at the moment that the projectile ceases to be acted upon by propelling forces. For a gunfired projectile the initial velocity, expressed as feet or meters per second, is also called "muzzle velocity." 3.17 Integral armor. Armor material used as part of a structure to perform a load-carrying or other operational function, in addition to ballistic protection. Also known as structural armor. 3.18 Lumiline screen. Photoelectric device used to activate or deactivate a chronograph upon passage of a projectile. 3.19 Muzzle velocity. The velocity of the projectile with respect to the muzzle at the instant the projectile leaves the weapon. This velocity is a function of the projectile weight, firing charge of the projectile, barrel characteristics, etc. See also "initial velocity." 3.20 Obliquity. A measure, normally in degrees, of the extent to which the impact of a projectile on an armor material deviates from a line normal to the target. Thus, a projectile fired perpendicular to the armor surface has 0 degrees obliquity. 3.21 Obliquity angle. Angle between the normal to the target surface and the projectile trajectory or line-of-flight. 3.22 Overmatch. A term used primarily in association with steel armor which indicates that the diameter of the impacting projectile is larger than the thickness of the armor plate. 3.23 Parasitic armor. See applique armor. 3.24 Penetration, complete (CP). A complete penetration occurs when the impacting projectile, or any fragment thereof, or any fragment of the test specimen perforates the witness plate, resulting in a crack or hole which permits light passage when a 60-watt, 1 10-volt bulb is placed proximate to the witness plate. MIL-STD-662F 3.25 Penetration, partial (PP). Any impact which is not a complete penetration shall be considered a partial penetration. 3.26 Petalling. The plastic deformation of a ductile material when struck by an impacting projectile or fragment, resulting in material being forced outward in leaflets or petal forms. 3.27 Projectile, fragment simulating. A projectile designed with special material, shape, and size for ballistic test firings so that the effect of typical fragments can be simulated. 3.28 Propellant. A rapidly burning substance or mixture whose combustion or release produces the gas pressure that propels the projectile through the gun bore. 3.29 Punching. Armor failure in shear where a circular plug about the size of the attacking projectile is pushed from the backside of the plate. 3.30 Sabot. Lightweight carrier in which a specified caliber projectile is centered to permit firing the projectile in the larger caliber weapon. The sabot diameter fills the bore of the weapon from which the projectile is fired. The sabot is usually discarded in flight a short distance from the muzzle, and only the subcaliber projectile continues downrange. 3.31 Small arms. All gas-propelled, tube-type weapons firing a ballistic projectile with a diameter up to and including 20 millimeters (0.787 inches). 3.32 Small arms ammunition. All ammunition up to and including 20 millimeters (0.787 inches). A round of ammunition includes a ballistic projectile, propellant charge, charge igniter (primer), and a charge case. 3.33 Spaced armor. Armor systems having spaces between armor elements. 3.34 Spalling. The detachment or delamination of a layer of material in the area surrounding the location of impact, which may occur on either the front or rear surfaces of the armor. Spalling may be a threat mechanism even when penetration of the armor itself is not complete. 3.35 Striking velocity. The velocity of a projectile or missile at the instant of impact (also known as impact velocity). 3.36 Target base line. The distance from a point midway between the two velocity measuring, triggering devices to the test sample. MIL-STD-662F 3.37 Terminal ballistics. A branch of ballistics which is concerned with the effects of weapons on targets including penetration, fragmentation, detonation, shaped charge, blast, combustion and incendiary effects. 3.38 Test sample. An armor plate or fabricated armor section or component which is to be ballistically tested for evaluation of ballistic protection properties. 3.39 Undermatch. A term used primarily in association with steel armor which indicates that the diameter of the impacting projectile is less than the thickness of the armor plate. 3.40 Vfio ballistic limit. In general, the velocity at which the probability of penetration of an armor material is 50 percent. 3.41 Witness plate. A thin sheet located behind and parallel to the ballistic test sample which is used to detect penetrating projectiles or spall. 3.42 Yaw. Projectile yaw is the angular deviation of the longitudinal axis of the projectile from the line of flight at a point as close to the impact point on the target as is practical to measure. 4. GENERAL REQUIREMENTS 4.1 Projectile. The test projectile shall be of the type and caliber specified in the contract. Millimeters shall be used to identify the caliber of projectiles unless otherwise specified. Table I provides the velocities (expressed in feet per second) of various projectiles at specific target distances. 4.2 Weapon. The weapon(s) used in the ballistic test firing shall be capable of firing the appropriate projectile at the specified V50BL(P) velocity range within yaw limitations. Millimeters shall be used to identify the caliber of weapons unless otherwise specified. 4.3 Velocity measuring equipment. 4.3.1 Chronograph. An electronic counter type chronograph measuring to at least the nearest microsecond (10"6 s) shall be used. 4.3.2 Detectors. Either high-velocity lumiline screens, or electrical contact screens which either open or close an electrical circuit by passage of the projectile through the detector shall be used. Contact screens may consist of metallic foils separated by a thin insulating layer, or may consist of a circuit printed on paper with the circuit spacing such MIL-STD-662F that the projectile passing through the screen will "break" the circuit. Chronograph or electronic timers used shall be calibrated and certified for accuracy. If accuracy is not certified, two pairs of velocity screens and two chronograph counters shall be used. This system enables the computation of an average projectile velocity between each pair of screens. The difference between the two instrumentation velocities shall be less than or equal to 10 ft s (3 m/s); thus, giving greater accuracy in actual average velocity. 4.3.3 Radar. Doppler radar is used occasionally to check lumiline screens. 4.4 Propellant. Any propellant which is either standard or suitable for the weapon shall be used. A projectile velocity-propellant charge curve for the weapon shall be determined before any testing is performed. This curve is required to provide a basis for selecting a powder charge to achieve a desired velocity. It is recommended that the propellant storage and weighing area be maintained at 19-24°C (65-75°F) and 50 + 5% relative humidity. 4.5 Test sample mount. The armor test sample shall be secured on the test target mount with impact side perpendicular to the line-of-flight of the projectile. The frame supports and clamps or mounting fixtures must be capable of retaining the sample and withstanding shock resulting from ballistic impact by the test projectiles. The test sample mount shall be capable of adjustment for moving the sample in the vertical or horizontal directions so that the point of impact can be located anywhere on the sample, and so that zero degree obliquity impacts can be achieved anywhere on the sample. The test sample mount shall be able to rotate on the vertical or horizontal axis so that various obliquity attack angles can be achieved. The test samples shall be mounted with a rigidity equal to or greater than the actual installation of the part. 4.6 Test sample. The sampling plan for ballistic acceptance tests shall be specified in the contract. 5. DETAILED REQUIREMENTS 5.1 Test conditions. Unless otherwise specified, all ballistic tests shall be performed in a standard atmosphere of 23 + 2°C (73 + 4°F) and 50 + 5% relative humidity. Temperature and humidity measurements shall be recorded for each firing. 5.2 Equipment setup. 5.2.1 Triggering devices. The spacing from the weapon muzzle to the first pair of triggering devices shall be sufficient to prevent damage from muzzle blast and obscuration from smoke in case optical devices are used. Recommended distances can MIL-STD-662F be found in ITOP 4-2-805. Spacing between triggering devices is a function of the expected velocity of the projectile being fired. In many instances, physical restriction, such as short overall distance from muzzle to test sample, dictates the spacing of the triggering devices. The last pair of triggering devices shall be placed at least 4 ft (122 cm) in front of test sample and should be protected from possible damage resulting from fragments. 5.2.2 Witness plate. The witness plate shall be 0.002 in. (0.05 mm) thick aluminum sheet for transparent armors and vision devices and 0.020 in. (0.51 mm) thick aluminum sheet for all other armors. The minimum size of the witness plate shall be 1 1 in. by I4 in. (279 mm X 356 mm) and be of sufficient size to be impacted by all fragments resulting from projectile penetration. The witness plate shall be made of 2024-T3, 2024-T4 or 5052 aluminum alloy sheet, and shall be located 6 + 0.5 in. (150 + 10 mm) behind and parallel to the armor test sample. When the test sample is a helmet the witness plate shall be rigidly mounted inside the helmet and 2 in. (51 mm) behind the area of impact and may be smaller than specified above so that it will fit inside the helmet. When the target presents a curved surface, such as a visor, the witness plate shall be located 6 + 0.5 in. (150 + 10 mm) behind the target, curved and oriented to maximize the probability of perpendicular impact. 5.3 Ballistic test procedure. The procedure listed below is a general description of the method for obtaining a V50BL(P). One should note that the actual method to be used may vary depending on target composition, specification or contract requirement. 5.3.1 Warm-up for constant velocity. When warmer rounds are needed for weapon or target alignment or establishment of a specific striking velocity, a test round shall be fired through the witness plate to determine the exact point of impact. Additional rounds shall be fired as required until the proper alignment and a stable striking velocity have been achieved. The propellant charge versus velocity curve for the weapon being used shall be referred to as a guide for establishing the required velocity within a practical + tolerance. Normally, this will be about + 25 ft s (8 m/s). 5.3.2 Yaw. The test sample shall be mounted as described in 4.5. The point of impact shall be located on the test sample and shall be positioned to line up with the previously determined line of flight of the projectile. Yaw shall be measured for each round by yaw cards, flash radiograph or photography. Any round for which yaw is determined to be greater than 5° shall be disregarded in the calculation of the ballistic limit. In the case of a dispute concerning a particular barrel, yaw shall be measured by a photographic measurement system using a multi-flash light source to determine projectile velocity and yaw. Yaw shall be measured by the system to an accuracy of 0.5 degree. MIL-STD-662F 5.3.3 First firing. For acceptance testing, the first round shall be loaded with a reference propellant charge so that the striking velocity is approximately 75 to 100 ft s (23 to 30 m/s) above the minimum required V50BL(P) as given by the appropriate specification. For most other types of ballistic tests, the first round shall be loaded with a reference propellant charge where the estimated likelihood of either complete or partial penetration is 50%. 5.3.4 Examination of witness plate. The witness plate shall be examined for penetration by holding it up to a light to observe light passage. A complete penetration is recorded when any light passes through the witness plate. If no light is visible through the witness plate, a partial penetration is recorded. 5.3.5 Subsequent firings. If the first round fired yields a complete penetration, the propellant charge for the second round shall be equal to that of the first round minus a propellant decrement for a 50 or 100 ft s (15 or 30 m/s) velocity decrease in order to obtain a partial penetration. If the first round fired yields a partial penetration, the propellant charge for the second round shall be equal to that of the first round plus a propellant increment for a 50 ft/s (15 m/s) velocity increase in order to obtain a complete penetration. A propellant increment or decrement, as applicable, for at least 50 ft/s (15 m/s) shall be used until one partial and one complete penetration is obtained. After obtaining a partial and a complete penetration, the propellant increment or decrement for 50 ft/s (15 m/s) shall be used. Firing shall be continued until a V50BL(P) is determined, using a random pattern of impact sites, unless otherwise specified. 5.4 Calculation of the V50 BUP) ballistic limit. The V50 BL(P) shall be calculated by taking the arithmetic mean of an equal number of the highest partial and the lowest complete penetration impact velocities within the allowable velocity span as defined by the contracting officer (see USATECOM TOP 2-2-7I0). 5.5 Computation of striking velocity. Instrumentation velocities shall be corrected as follows: Vs = V, - VL Where: Vs = Striking velocity at the test sample V| = Instrumentation velocity = Distance (between sensory devices) Time (chronograph reading) MIL-STD-662F VL = Velocity loss (over target base line) Velocity loss is calculated in accordance with the following formula: VL = (XG Drel)/C Where: X = Distance from baseline to target G = Drag factor (can be obtained from APG per ITOP 4-2-805, Appendix F). Drel = Relative air density C = Ballistic coefficient^ per ITOP 4-2-805, Appendix F). 5.6 Ballistic test report. Ballistic test reports shall contain the following minimum information as applicable: a. Contractor identification. b. Test facility. c. Contract number. d. Lot numbers and quantities. e. Item specification number. f. Armor material description. g- Material identification number for each test sample. h. Temperature and humidity at the test facility. i. Date. j- Personnel conducting test and any witnesses. k. Weapon used. 1. Projectile used. m. Projectile weight, grains. n. Type of propellant. 0. Weight of propellant for each shot, grains. P- Impact velocities used in computing V50's with highest partial penetration lowest complete penetration, range (spread), and velocities of all rounds, q. Witness plate characteristics, partial or complete, r. Calculated V50BL(P) ballistic limit. s. Remarks pertinent to the conduct of the test, or behavior of the material. MIL-STD-662F Additional data may be required by a contracting activity. When testing is done at a place other than a Government facility, results shall be reported on forms either furnished or approved by the Government. One copy of each complete report shall be forwarded to the agency designated by the Government. 5.7 Acceptance and rejection. The selected armor samples shall meet the minimum V50BL(P) ballistic requirements specified in the order for the represented lot to be acceptable. Failure of any test samples to meet the minimum specified V50BL(P) ballistic limit shall constitute rejection of the entire lot which they represent. Unless otherwise specified, the ballistic tests shall be conducted and the test results accepted prior to shipment of the lot of armor represented by the test samples. 5.8 Test samples ownership. Ballistic test samples that comply with ballistic requirements are considered as part of the lot of armor they represent, and ownership of them passes to the Government upon acceptance. The Government inspector shall dispose of these test samples unless instructed otherwise by the procuring activity. Test samples that fail to comply with the ballistic requirements are considered as part of the lot they represent and remain the property of the supplier just as does the rejected lot they represent. 5.9 Retests. Reference shall be made to the appropriate specification or applicable test directive for guidance on the number of retest samples required, if such are allowed. If the retest samples do not pass the ballistic test, the lot from which they came, or the process by which they were made shall be permanently rejected. Otherwise, if all retest samples pass, the lot or process shall be accepted. 5.10 Security classification of armor. Terminal ballistics performance data on armor materials shall be classified in accordance with ARL PROGRAM No. 0183009, "Security Classification Guide for Armor Materials" dated 30 July 1993. 6. NOTES (This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.) 6.1 Intended use. This test method standard is military unique because it is intended for use in ballistic acceptance testing of armor and for research and development of new armor materials (see 1 .2). MIL-STD-662F ject term (key word) listing. Projectile Propellant Weapons anges from previous issue. Marginal notations are not used in this revisionanges with respect to the previous issue due to the extent of the changes. MIL-STD-662F TABLE I. Projectile velocities (feet second). MIL-STD-662F TABLE I. Projectile velocities (feet second) (cont.). REMAINING VELOCITY (F/S) AT SPECIFIC DISTANCE REMAINING VELOCITY (F/S) AT SPECIFIC DISTANCE MIL-STD-662F TABLE I. Projectile velocities (feet second) (cont.). REMAINING VELOCITY (F/S) AT SPECIFIC DISTANCE MIL-STD-662F CONCLUDING MATERIAL Custodians: Preparing activity Army - MR Army - MR Navy - MC Air Force - 1 1 Project 8470-0169 Review activities: Army - AR, AT, AV, GL, IE, TE Navy - CG, NU Air Force - 03, 45, 82 DLA - CT DOT - CGCT O Form 1426. OCT Previous editions ire ocsoete. In some embodiments, a single ply of fabric has a V50 value of at least 700 fps for a 2 grain projectile. In some embodiments, the V50 value for a single ply is at least 900 fps and in some embodiments the V50 value for a single ply is over 1000 fps, inclusive. A double ply of some fabric embodiments can have even higher V50 values, some over 1100 fps, inclusive. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic fibers and secondary fibers, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, this knitted fabric layer also includes stretch yarns. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic spun yarns having no more than 95% ballistic fibers, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes at least two different ballistic fibers, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, this knitted fabric layer includes ballistic yarns comprising the at least two different ballistic fibers. In a still further embodiment, these ballistic yarns are spun yarns. In some embodiments, a single-ply knitted fabric layer (i) includes at least two different ballistic fibers, (ii) has a weight between 2.5-11 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes at least two different ballistic fibers, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 900 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic spun yarns and secondary yarns, (ii) has a weight between 2.5-10 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic yarns, secondary yarns, and stretch yarns (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, the ballistic yarns of this knitted fabric layer are spun yarns. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic yarns and stretch yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, the ballistic yarns of this knitted fabric layer are spun yarns. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and secondary yarns, (ii) has a weight between 2.5-11 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and secondary yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 900 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and stretch yarns, (ii) has a weight between 2.5-11 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and stretch yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 900 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and ballistic spun yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and ballistic spun yarns, (ii) has a weight between 2.5-11 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns and ballistic spun yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 900 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns, ballistic spun yarns, and stretch yarns, (ii) has a weight between 2.5-11 osy, inclusive, and (iii) has a V50 value greater than 700 fps. In some embodiments, a single-ply knitted fabric layer (i) includes ballistic filament yarns, ballistic spun yarns, and stretch yarns, (ii) has a weight between 2.5-12.5 osy, inclusive, and (iii) has a V50 value greater than 900 fps. The following single ply ballistic fabrics having the disclosed blends and constructions were tested pursuant to the V50 Ballistic Test. TABLE 1 These single-ply ballistic fabrics were tested as 15 inch square samples pursuant to the 2 grain RCC ("right circular cylinder") V50 Ballistic Test, in a rigid frame and backed by air. The V50 number notes the velocity (in feet per second) at which the probability of penetration of the fabric by the projectile is 50 percent. In this table, the symbol " | " denotes a fabric that has a different blend for its technical face and technical back. In this table, the symbol " | | " denotes a fabric that has two yarns of different blends oriented such that the first yarn is exposed on the technical face and technical back of the fabric and the second yarn is embedded in the fabric. The blend to the left of the symbol is the fabric with which the testing projectile first comes in contact when striking the fabric. Dyeing and printing of the disclosed fabrics may be carried out in accordance with standard methods, all of which are known to those of skill in the art. Any of the fibers disclosed herein may be producer-colored in that color is imparted to the fibers during the fiber formation process. Embodiments of the ballistic fabrics disclosed herein may be incorporated into a variety of different garments in various ways. Such garments may include, but are not limited to, shirts, pants, protective undergarments, gloves, knee and elbow pads, jumpsuits, t-shirts, etc. The entirety of the garments may be formed from the inventive fabrics, or alternatively such fabrics may be incorporated into the garments at strategic locations. In one embodiment, the entirely of the garment is formed of the fabric (e.g., protective undergarments). In other embodiments, pockets or enclosures are provided on the exterior or interior of the garment in strategic locations (e.g., the forearms, groin area, femoral arteries, etc.). The ballistic fabric is positioned within the pockets as protective inserts to stop penetration of the ejecta through the garment. The ballistic fabrics may be provided as inserts that are removable and replaceable in the pockets. Placement of the pockets on a garment may be customized depending on the task of the wearer and not all pockets need be filled with protective inserts. Furthermore, different types of protective inserts may be available. In this way, the protection afforded the wearer by the garment may be customized and tailored to a particular situation. In other embodiments, the garment is constructed so that the ballistic fabric forms desired portions of the garment. By way only of example, the arms of the garment may be formed from ballistic fabrics disclosed herein. Alternatively, panels or patches of fabrics disclosed herein may be adhered, sewn, or otherwise attached to an existing garment at desired locations. Still further, the ballistic fabric may be supplied in a layer or film that is attached (such as via adhering, stitching, laminating, etc.) to the fabric at the desired locations. The foregoing is provided for purposes of illustrating, explaining, and describing embodiments of the present invention. Further modifications and adaptations to these embodiments will be apparent to those skilled in the art and may be made without departing from the scope or spirit of the invention. Different arrangements of the components depicted in the drawings or described above, as well as components and steps not shown or described are possible. Similarly, some features and subcombinations are useful and may be employed without reference to other features and subcombinations. Embodiments of the invention have been described for illustrative and not restrictive purposes, and alternative embodiments will become apparent to readers of this patent. Accordingly, the present invention is not limited to the embodiments described above or depicted in the drawings, and various embodiments and modifications can be made without departing from the scope of the claims below.