AU5932998A - Materials for shock attenuation - Google Patents

Description

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COMPLETE SPECIFICATION STANDARD PATENT

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Applicant(s): Address for Service: Invention Title: Cemcon Corporation 4100 Pistoria Road Baltimore Maryland 21229 UNITED STATES OF AMERICA DAVIES COLLISON CAVE Patent Trade Mark Attorneys Level 10, 10 Barrack Street SYDNEY NSW 2000 Materials for shock attenuation The following statement is a full description of this invention, including the best method of performing it known to me:- 5020 MATERIALS FOR SHOCK ATTENUATION BACKGROUND OF THE INVENTION This invention relates to shock attenuating chemically bonded, ceramic materials which exhibit a combination of properties which make them particularly useful in applications where shock attenuation is of significant importance, in environments where the materials are subject to shock waves from explosives or from seismic sources, and particularly for magazine construction, or as materials for security walls and doors, or for the construction of buildings resistant to a strong blast, depending on the porosity and on the .I density of the materials. More particularly, it relates to chemically bonded S 10 ceramics which have densities that range from 30 to 160 lb/ft 3 (0.48 to 2.56 o g/cc) and porosity of 20% to The low density materials display excellent weight efficiency while the higher density systems are the most space efficient shock attenuating materials available particularly in strong shock environments. These features coupled with their relatively low-cost, easy formability and non-flammability make them very well suited to ammunition storage applications. The range of porosity, density and strengths that are available allow them to be tailored to specific ammunition storage applications or blast resistant barrier designs.

A discussion of the development of and the properties desired in such materials is found in a paper entitled, "Development of Shock Absorbing Barrier Materials For High Performance Magazine Construction" by Claudio Herzfeld and Sean Wise, presented at the 26th Explosives Safety Seminar, sponsored by the Department of Defense/Explosive Safety Board on August 16-18,1994. The contents of this paper are incorporated in this application by this reference.

SUMMARY OF THE INVENTION One object of the invention is to provide new materials which attenuate shock.

Another object of the invention is to provide shock attenuating materials which provide ballistic protection in an ammunition storage environment.

A further object is to formulate chemically bonded ceramics materials in which the density, strength and porosity are controlled to provide shock attenuating properties which are more space efficient than previously known materials.

10 A further object is to provide compositions which are relatively low in cost, possess easy formability, and non flammability and which are formulated from readily available materials.

This invention is an improvement over the light weight cementitious S:compositions described in one or more of the following recently issued United States patents, the disclosures of which are incorporated by this reference: :°ooo, Miller et al. 4,501,830 issued February 26, 1985; o Rizer et al. 4,504,320 issued March 12, 1988; Wise et al. 4,599,211 issued July 8, 1986; and Double et al. 4,780,141 issued October 25, 1988.

As described in these patents, cementitious compositions comprising Portland cement, silica fume, fillers, dispersing agent and other additives may be produced with properties useful for a variety of purposes.

The present invention is directed to improved novel compositions which produce products having densities that range from 30-160 pounds per cubic foot (.048 to 2.56 g/cc) and porosities of 20% to 80%. These materials were found to be excellent shock attenuating materials and to exhibit a high degree of space efficiency. Sympathetic detonation of class 1.1 munitions is one of the most severe hazards associated with munitions storage as well as one of the most difficult to control. Traditionally, quality distance (QD) requirements have been employed to mitigate the hazards to personnel and property but this reduces the explosive weight of munitions stored in a given storage location and increases operational costs. Realizing the benefits of reducing the sensitivity of munition to unplanned stimuli, the military has established insensitive munitions (M standards for new weapon systems in Mil Std 2105A. These standards address impact by shaped charge jets, fragments, bullets, and spall, slow and fast cooloff as sympathetic detonation. Methods and design strategies for high performance ordnance items have been developed that provide acceptable response to most of these unplanned stimuli with the exception of sympathetic S. 15 detonation. In this latter case, explosive fills that display reduced sensitivity to **sympathetic detonation often have unacceptable performance so they are rejected by the user.

Packaging solutions to the sympathetic detonation problem using the #eo.

materials of this invention can overcome the IM- performance trade-off.

BRIEF DESCRIPTION OF THE DRAWINGS The invention will be better understood from the description which follows taken in conjunction with the drawings in which: Figure 1 is a graph showing a range of strength versus density of materials of this invention as compared with strength versus density of traditional prior art cement based systems; Figure 2 is a generalized Hugoniot in stress volume space; Figures 3A through 3E are a series of drawings showing the response of the materials of this invention to impact by a high speed steel plate creating a very strong shock; Figures 4A through 4E are a series of figures showing a generalized view of gage traces in a compacted SA/CBC target showing spread of load and attenuation of peak pressure; Figures 5, 6 and 7 show High Stress rate test results for various SA/CBC materials plotted as Stress vs. Velocity (Fig. Stress vs. Volumetric Stress (Fig. and Stress vs. Specific Volume (Fig. 7); Figure 8 shows experimental or calculated depth of penetration into SA/CBC material; and Figure 9 shows deformation of projectiles recovered from impacted SA/CBC as a function of target density and initial projectile velocity.

."DETAILED DESCRIPTION OF TmHE PREFERRED EMBODIMENT 15 All of the SA/CBC (shock attenuating/chemically bonded ceramics) formulations of this invention contain Portland cement, silica fume, and hollow fillers. Usually, the hollow filler is a coarse particle relative to the cement and is essentially inert. Hollow fillers useful in this invention include, glass bubbles, mineral bubbles and a manufactured multicellular bubble. In addition, many of the formulations contain some sort of fiber, either organic, glass or metal. The organic is used to control the response of the material to fire (it prevents spalling), glass is used for toughening and improving tensile strength while metal (steel or stainless steel) is used for toughening and increasing the density.

The materials of this invention are all porous and may be grouped by density and strength. As shown in Figure 1. All the strength to density ratios obtained are at least a factor of 2 higher than for traditional lightweight mortars and concretes. The first group are the lightest weight formulations with densities of 30 to 65 pound/ft 3 (0.48 to 1.05 g/cc). Their compressive strengths range from 1500 psi to 7,000 psi, while their calculated pore volumes range from 50% up to 80%. The second or middle density group have densities in the range of 65 to 110 pound/ft 3 (1.05 to 1.75 g/cc) and have compressive strengths in the range of 7,000 psi to 15,000 psi. The porosity of these systems is in the range 35 to 50 percent. The third or high density group have densities in the range of 110 to 160 pound/ft 3 (1.75 to 2.6 g/cc) and have compressive strengths of 15,000 psi to nearly 30,000 psi and are still quite porous. Most of the products of the high density group have a minimum 20 percent porosity before drying and all have in excess of 40% porosity after drying. The combination of strength, density, and porosity makes each of these systems very effective at attenuating strong shock and providing ballistic protection.

0 The attenuation of a shock in the SA/CBC materials of this invention is related to strength, porosity and density. Typically, these porous materials undergo a loading mechanism leading to even more rapid reduction in magnitude S 15 of the peak stress as the plastic wave transitions through the material. Finally, when the stress in the plastic wave drops below that of the Hugoniot Elastic Limit (HEL), the stress will be transmitted as it would in any other non-porous material without plastic deformation. High strain rate test results are shown in Figures 5, 6, and 7 for selected SA/CBC materials in Stress-Velocity, Stress- Volume and Stress-Specific Volume projections. In these Figures the relatively high dynamic strength of the materials coupled with their high plastic strain capability are clearly visible.

Controlling the HEL can be used to limit the impact forces on either a target or a projectile. If the impact velocities are low enough such that an overdriven shock wave will not be imparted to the target material, then the maximum impact pressure will be near the HEL so long as the porosity is not completely crushed out of the SA/CBC. If the HEL then is well below an explosive's initiation threshold, it will not be initiated from this impact.

Besides attenuating shocks, the shock attenuating chemically bonded ceramics (SA/CBC) of the invention provide good resistance to penetration of high speed fragments. Fragment impact testing revealed that depth of penetration (DOP) into the SA/CBC and fragment deformation are functions of the density and the compressive strength of the target material. The DOP was found to be more strongly correlated to the strength of the target material at low speed 1.0 km/sec) while the fragment deformation is very strongly related to the target density, particularly at high speed 1.5 km/sec.) An expression that accounts for target material's strength and density as well as projectile's velocity is the Poncelet equation which was used to analyze SA/CBC's ballistic penetration data.

The Poncelet equation defines the intrafacial forces F, between the fragment and the target as a function of the target material's compressive strength, y, density, p, projectile velocity, v, and impact area A as shown in the equation. The Cly term in this equation is the force acting on the projectile due to the target material's strength while the C 3 pv 2 term is the drag force acting on the projectile.

F ma -(Cly C 3 pv 2 )A Poncelet Equation From this equation, a second expression can be derived that shows the depth of penetration, x, as a function of the material parameters and the projectile mass and initial velocity as shown in the equation below: m Cy Cp x M In v 2 1 3 2 C3pA 1 C3p C y DOP Equation derived from Poncelet Equation Through a series of ballistic tests in which fragments were shot at thick samples of a variety of SA/CBC targets, a value for C, of 5.4 was found along with a value of 0.6 for C 3 The DOP equation derived from the Poncelet equation provides a very good prediction of penetration into SA/CBC targets so long as the projectile does not deform (see Figure In addition, the interfacial force calculated using the drag term of the Poncelet equation are proportional to the deformation found in fragments shot at high speed into the SA/CBC (see Figure 9).

.The ballistic data and subsequent analysis show that density accounts for 10 much of the SA/CBC's penetration resistance to fragments at very high speeds.

:-.The Poncelet equation suggests that the density accounts for 75% of the force acting on a projectile traveling through a SA/CBC material at 1830 m/s a(6000 ft/s) and 85 of the force acting on a projectile at 2300 m/s (7500 ft/s).

The density is also primarily responsible for projectile deformation which can lead to substantially lower depth of penetration. Impacts at these speeds create ~an overdriven shock in the SA/CBC.

The strength is the dominant factor in bringing the fragments to a stop once velocities are less than 1000 m/s (3000 ft./sec). Surprisingly, the pore content does not directly figure into the calculations. Pore content is still an indirect factor in that the total porosity will affect the density and the mechanical strength. The effect of porosity on strength can be minimized, however, if the pores are made small enough as was done with the S8 formulations described below. In fact, the best material ballisticly was dried S8 which had a pore content of 43 Using the high strain rate characterization data from the SA/CBC materials it is possible to assess their performance in different environments and determine what materials are suitable to different applications. The paragraphs below review these grouped into differing density regimes.

The lightest materials of this invention are intended to be used in weak shock environments such as those where there is a relatively small amount of explosive in a given volume or where impact velocities are quite low. Examples of these materials are set forth in Table 1. The lightest weight material in Table 1 is the formulation labeled GC2 with a density under 40 lb/cu. ft. It provides shock absorbtion and ballistic resistance to fragments for 40mm grenades in a storage container separated by less than 1.25 inches of material. The material 10 also provides thermal insulation in case of fire.

Formulations S6 and MBW 60 have been used as an integral part of a barrier separating stacks ammunition. The function of the material was to act as a cushion on the face of the wall. If a detonation occurred in one storage cell, the barrier wall would stop the high velocity fragments in its core but would be 15 pushed out into the stacks of ammunition in other cells. The SA/CBC cushion is designed to prevent a hard impact with the ammunition and cause it to detonate. These impacts are less than 200 m/s. The strength range of the 9999 SA/CBC has upper and lower limits in order for the wall to perform its function.

Manufacturing quality control combined with the design of the formulations allow this level of performance to be achieved. This principle was successfully demonstrated earlier this year. The material helps provide a cost effective solution for magazine construction which will allow more ammunition to be stored safely in a limited area.

The light weight materials of Table 1 have significant commercial potential beyond ammunition storage. They could be used as structural insulation for fabrication of low rise story) buildings or as an energy absorbing material in buildings subjected to seismic loading or blast loading.

The use of an SA/CBC material such as those in Table 1 may provide a means to keep the loads on a structure within a manageable level, even for severe attacks such as the one in Oklahoma City.

Examples of the medium density porous materials of this invention are shown in Table 2. These materials provide exceptional strength at moderate density. They have significant resistance to impact from fragments, bullets and hammers because of their high compressive strength yet still provide good shock absorbing capabilities. These systems provide a good balance of weight efficiency in ammunition storage coupled with ballistic protection. The combination of strength, density and porosity make them suitable for security :'o":applications such as walls and doors where good penetration resistance at low 4. 4barrier weight is a critical issue.

Table 3 sets forth examples of high density SA/CBC materials of this invention. They provide maximum strength, density and porosity in most cases). High performance cement based systems previously have been made with strengths and densities of 25,000 psi at a density of 150 pound/ft 3 (respectively) but these are made with minimal porosity. The high density

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SA/CBC systems are the most volume efficient materials in a very strong shock environment (>30 kbars) and hence are suitable for barriers that have to perform in a limited space. The ballistic weight efficiency of the highest strength systems in this set is nearly equivalent to aluminum for very high speed fragments.

The pore system in these high density mixes is extremely fine. The closed cell pore system is made from a 10 micron hollow particle (55% void volume) called "Sphericell 110 P8" that has a hydrostatic crushing strength of nearly 20 kpsi. A high volume fraction (0.45) of these particles is packed into the S8 formulation producing about 25 of the total porosity in the mix. With a water/cement ratio of 0.55, a compressive strength of 20-25 kpsi is obtained once the water is removed by thermal treatment. These sphericell hollow fillers are also included in the highest density SA/CBC formulations. In these, however, a water/cement ratio of 1.44 is used in order to create additional void volume when dried. Even with this exceptionally high water content, compressive strengths of 15 kpsi are obtained, leading to speculation that the particle may be acting as pozzolanic materials.

As seen from Tables I, II and III, discussed above, the shock attenuating, chemically bonded ceramic materials of this invention comprise the following: 10 A. Portland cement D. dispersing agent silica fume E. other additives, and C. hollow fillers F. water S"A. Portland Cement Any of the various grades of Portland cement described in the above 15 noted U.S. patents are suitable for the present invention. Too much cement increases the product density and too little cement yields products which are too weak. In the examples which follow, LWPC refers to Lehigh White Portland Cement. The amount of Portland cement is usually between about 6% and about by weight.

B. Silica Fume The chemically active silica fume used in the mixtures which produce the cementitious composite materials of this invention is preferably an amorphous, non-crystalline, pozzolanic silicon dioxide and is preferably condensed silica fume. This condensed silica fume is produced as a byproduct in the electric arc furnace production of silicon or silicon alloys such as ferrosilicon. The gases which are evolved during the manufacture of ferrosilicon from quartz, coke and iron ore when they are heated to about 20000 C, contain Si and SiO vapors which form SiO 2 when they react with air as they emerge from the furnace.

These vapors condense and the very tiny spherical particles which result from condensation of the vapors are almost entirely amorphous silica with a 15-20 m 2 /g surface area. Typically, the particles analyze 85-92% SiO 2 and the remainder being small amounts of alumina, lime and magnesia. The particles range from 0.01 to 0.3 micron with about 70% being smaller than 0.1 micron.

This material is described in U.S. Patent Number 4,321,243, issued March 23, 1982.

This constituent is believed to have pozzolanic properties in the present to0 compositions. Although in itself it possesses little or no cementitious value, at :ordinary temperatures, in the presence of moisture, it will chemically react with calcium compounds to form compounds possessing cementitious properties.

C. Hollow Filler Any of a wide variety of hollow fillers may be used in the formulation of the present invention, including glass bubbles, mineral bubbles, and a manufactured multicellular bubble. One particularly preferred hollow filler is the fly ash cenospheres which are commercially available as Fillite (RTM) and are described in U.S. Patent No. 3,782,985. Another preferred hollow filler is the silicous spheres sold as spherical 110P8. A third suitable filler is a glass bubble obtained from 3M called Scotchlite (RTM). It is available in densities that range from approximately 10 Ib/cu ft (0.15 g/cc) to 40 lb/cu ft (0.6 g/cc).

D. Dispersing Agent The compositions of this invention include a dispersing agent or plasticizer in the formulations. One such dispersing agent used to make the mixture more fluid is sold as Mighty 100 or Mighty 150, in which the active ingredient is the sodium salt of the formaldehyde condensate of naphthalene beta sulfonic acid. Other similar materials may be used as dispersing agents.

E. Other Ingredients The inclusion of a fiber improves the properties of many of the compositions of this invention. The fiber may be either organic synthetic resin polymer) or inorganic glass or metal). Combinations of fibers may be used. It has been found that glass fibers are useful for toughening and increasing the tensile strength of the material while metal such as steel or stainless steel also toughens the product and increases the density.

F. Water The density and porosity of the final product are influenced by the amount 10 of water in the formulation. For low density products the amount of water is preferably between 20% and 35%, for medium density it is between 10% and 20%, and for high density between 9% and 13%. The relative proportions of the other ingredients may be varied depending on the density and porosity desired in the final product. Suitable ranges are given in Table 4.

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99 9 4 *9 9 99 4 *9 99 .9 TABLE 1: LOW DENSITY MATERIALS 33.34 7.841 LWCP 37.38 11.11 LWPC Type 11 34.07 10.21 Type III 16.67 5.88 11.65 5.19 10.8 4.06 11.52 4.78 1.25 0.58 M-100 1.03 0.63 M-100 0.7 0.41 Meiment 0.93 0.62 Borem, HSP 33.34 1 24.7 24.29 22.72 26.6 21.98 24.66 23.26 0.01 0.01 Pozzolith 12.15 60 C15/250 24.32 0.38 B38/4000 14.8 38.22 Microlite T 15.1 42 irlt 10.9 Ext. SG 12.39 16.24 Ext. SG 0.53 15 Foam 3-24 1 0.25" AR 1.28 0.5 1/4"AR 1.6 0.54 0.5" E glass 1.55 0.61 0.5"E glass 0.1 0.08 microfiber 0.06 0.05 microfiber J 2 100 0.65 3.211 31 1 0.751 3.281 80f 0.721 3.051 78% 0.73 0.61 0.88 0.84 0.8 0.99 2000 6900 1500 5E+05 2800 8E+05 610 300 6EI-05 500 8E+05 0.1 0.08 0.1 0.1 TAL 11 MEDAUM. DENSITW:MATERIAiLS Formulation Ingredients Cement Silica Fume Water Disp. Agent Bubble 1 GC2 IS2 I S3 I I I I-I~ r I I I I 1U4 1 L18 jVQI.7/O T ype wt.% Vol.% Type wt.% Vol.% Type Wt.% Vol. %vo 35.18_ 17.1 LWC., 26.16, typeL P 2.4 1 .7 W C Wt%? Vol.'/ Type 351 1.1 WP 616 1.4 WP 2.4 124 LWC 27.81 13.09 LWPC 30.31 15.13 LWPC 36.93 20.29 LWPC 16.29 11.81 12.04 8.62 20.5 11.9 11.01 7.77 18.66 14.12 18.17 14.3 13.45 20.48 14.39 21.62 18.12 22.07 19 91 36 14 32 1.23 1.18 M-100 0.91 0.88 M-100 1.15 0.88 Mi00 0.84 0.77 M0 .6 10 iO 12 .9 M0 189 Ar AO Cl .0 10 1 .9 1.9 M0 10000 ZU.U 51I.42 S60/ 25.32 51.42 S60/ 16.65 41.15 S60/ 20.03 16.68 Ext.

100000 20.032- -I Bube29.72 13.1 Shercell Fiber 1 15.36 3 4345S 29.52 5 434 SS 1.97 1 .05" AR 2.28 1.38 0.5" 16.12 3.25 434SS 13.64 3 0.5' Ri gla AR gla Brass Coated Fiber 2 18.83 3.58 434SS Properties W/C OPC/SF Flow 0.38 2.17 65 0.55 2.17 60 0.55 1.61 44 0.46 2.52 29 0.44 1.61 68 0.38 2.03 59 Pore Volumne% 35% 39% 39% 36% 32.4% 46.4 27.36 46

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Density 1.54 1.54 1.22 1.52 1.57 1.44 1.77 1.59

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g/cc Hyd Camp. a (psi) 15000 12500 110250 12500 13000 16000 E (Mpsi) Dehyd. Camp. s 14900 17000 (psi) E (Mpsi) Hyd. Flex. a (psi) 2100 1.76 2700 1700 1.38 3200 1.46 2100 1.86 E (Mpsi) Dehyd. Flex. s 2340 1.25 4500 0.7 (psi) E (Mpsi)I Shrinkage 0.1 0.08 0.9 0.6 0.1 0.1 (Hyd.) Shrinkage 0.2 0.2 (DeHyd)

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*9 9 9 9 TkBLE 0 III:* HIGH 9*9 9 999 9 9 9 99 99 99 9 9* 999 9* 99 9 99 9 9 *9 4~N~ITY~ MAfl7E1IlA~kS *Formulation S8 LC S8 High p Pourous Ingredients wt.% Vol.% Type wt.% Vol.% Type wt.% Vol.% Type Cement 1 20.26 12.89 1839 11.59 Class H 7.92 6.67 LWPC Cement 2 2.03 1.3 Type K Silica Fume 12.56 11.99 12.56 11.98 4.91 5.92 Water 10.73 21.49 10.74 21.51 11.41 30.26 Disp. Agent 0.82 1 03 M100 0.82 1.03 0.39 0.65 Mi00 Bubble 1 24.48 44.6 Sper. 11OP8 24.49 44.6 Sper. 110OP8 14.93 36 Sper. 11OP8 Other Filler 41.16 14 Iron Sponge Fiber 1 31.14 8 434SS 31.15 8 S 2070CS 19.25 6.5 434SS Properties W/C OPC/SF Flow 0.53 1.61 36 0.153 1.61 48 1.44 1.61 88 Pore Volume 25% 43% 25% 43% 20% 44.2% Density (HOD) g/cc 2.1 1.9 2.1 1.9 2.8 2.53 Hyd. Comp. a (psi) E (Mpsi) 19000 17000 9000 Dehyd. Comp. s (psi) E 22000 26500 19000 (Mpsi) Hyd. Flex o (psi) E (Mpsi) 4350 Dehyd. Flex s (psi) E (Mpsi) 4000 0.9 Shrinkage (Hyd) 0.06 Shrinkage (DeHyd) 0.13 TABLE IV: PROPORTIONS BY WEIGHT High Density Medium Density Low Density Portland Cement 6-21 25-40 33-40 Silica Fume 4-13 10-20 8-18 Hollow Spheres 14-25 15-30 10-30 Water 9-13 10-20 20-35 Plasticizer 0.3-0.9 0.5-1.5 0.5-105 Fiber 15-35 1-20 0.05-5 Water/Cement 0.5-1.5 0.35-0.65 0.6-1.1

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Having now described the preferred embodiment of the invention, it is not intended that it be limited except as may be required by the appended claims: Throughout this specification and the claims which follow, unless the context requires otherwise, the word "comprise", or variations such as "comprises" or "comprising", will be understood to imply the inclusion of a stated integer or step or group of integers or steps but not the exclusion of any other integer or step or group of integers or steps.

Claims (20)

1. A shock attenuating material having a density from about 30 to 160 lb/cubic foot and a porosity of about 20% to 80% and a compressive strength between about 500 and 30,000 psi.

2. The material of claim 1 wherein the density is from about 30 to lb/cubic foot, the porosity is between about 50% and 80% and the compressive strength is between 500 psi and 7000 psi.

3. The material of claim 1 wherein the density is from about 65 to 110 lb/cubic foot, the porosity is between about 35% and about 50%, and the compressive strength is between about 5,000 psi and 15,000 psi.

4. The material of claim 1 wherein the density is from about 110 to about 160 lb/cubic foot, the porosity is at least about 20%, and the compressive strength is between about 15,000 psi and about 30,000 psi. A shock attenuating chemically bonded ceramic material having a density from about 30 to 160 lb/cubic foot and a porosity of about 20% to and a compressive strength between about 500 and 30,000 psi.

6. The material of claim 5 wherein the density is from about 30 to lb/cubic foot, the porosity is between about 50% and 80%, and the compressive strength is between 500 psi and 7000 psi.

7. The material of claim 5 wherein the density is from about 65 to 110 lb/cubic foot, the porosity is between about 35 and about 50% and the compressive strength is between about 5000 psi and 15,000 psi.

8. The material of claim 5 wherein the density is from about 110 to about 160 lb/cubic foot, the porosity is at least 20% and the compressive strength is between about 15,000 psi and about 30,000 psi.

9. A mixture from which high porosity materials for shock attenuation can be cast, said mixture comprising the following in percent by weight. Portland cement 6 to Silica Fume 4 to Hollow Filler Particles 10 to Fibers 0.05 to Water 9 to 35; and o Plasticizer up to 2.

10. A mixture according to claim 9 wherein the relative proportions in weight percent are: Portland cement 6-21, silica fume 4-13 Hollow Filler Particles 14-25, fibers 15-35 Plasticizer .03-.09 and water 9-13.

11. A mixture according to claim 9 wherein the relative proportions in weight percent are: Portland cement 25-40, silica fume 10-20 Hollow Filler Particles 15-30, fibers 1-20 Plasticizer 0.5-1.5 and water 10-20.

12. A mixture according to claim 9 wherein the relative proportions in weight percent are: Portland cement 33-40, silica fume 8-18 Hollow Filler Particles 10-30, fibers .05-5 Plasticizer 0.5-1.5 and water 20-35.

13. A mixture according to claim 9 wherein the fibers are selected from the group consisting of organic fibers, glass fibers and metallic fibers and mixtures thereof.

14. A mixture according to claim 9 wherein the fibers are organic. 9 4 A mixture according to claim 9 wherein the fibers are glass fibers. @9*

16. A mixture according to claim 9 wherein the fibers are metallic. .4*

17. Shock attenuating articles produced by casting a mixture of claim 9, and 9* 9 permitting the mixture to set or harden.

18. Shock attenuating articles produced by casting a mixture of claim 9 and dehydrating the article after it has set.

19. Shock attenuating magazines or ammunition storage racks produced by the process of claim 17. Shock attenuating building components produced by the process of claim 17. P:\WPDOCS\PAT\CLAIMS\679800.WPD 17/3/98

21. A shock attenuating material substantially as hereinbefore described with reference to the drawings.

22. Shock attenuating articles, substantially as herein described with reference to the accompanying drawings.

23. A process of producing shock attenuating articles, substantially as herein described. DATED this 17th day of March 1998 S :CEMCON CORPORATION :By Its Patent Attorneys DAVIES COLLISON CAVE Se *0