Abstract:
A new arrangement of matter is developed which can be formulated to be a high explosive, a propellant or a gas generator. The new arrangement of matter in its explosive embodiment is known as a microknit composite explosive (MCX) in which an essentially anhydrous mixture of inorganic salts, surfactants and organic fuels is prepared while the oxidizer is molten, and a microcrystalline property is created which imparts a hard, machinable characteristic to the arrangement of matter. The invention includes three processes for making MCX compositions: (1) dissolving surfactants, crystal-habit modifiers, thickeners or combinations into the molten oxidizer in a manner which permits supercooling with subsequent solidification; (2) forming an unstable oil-continuous emulsion as a preliminary step, followed by a controlled disruption of the oil-phase continuum which causes the composition to solidify after supercooling, and (3) retarding crystal nucleation in salt-continuous emulsions by introducing surfactants, thickeners, crystal-habit modifiers or combinations, along with immiscible fuels, resulting in supercooling and subsequent solidification to a hard composition.

Description:
BACKGROUND OF THE INVENTION 
     Explosive compositions may be divided into two categories: molecular or homogeneous explosives, wherein the molecule of the compound contains chemical moieties which confer explosive properties, and composite or heterogeneous explosives wherein mixtures of fuels and oxidizers can be made to be explosive. 
     Composite explosives are made by mixing oxidizing salts, usually perchlorates or nitrates, with appropriate amounts of organic or metallic fuels. Many useful explosives are thus made, and it has been found that such mixtures are improved in utility and performance by formulating the mixtures as slurries or emulsions, which improves the intimacy of contact between the fuel and oxidizer. Further, such compositions are pumpable, which greatly facilitates their manufacture and placement for use. 
     Another type of composite explosive is made by mixing two or more molecular explosives. Typical of these are melt-cast formulations which are widely used as fills for military explosive ordinance. A commonly used explosive mixture is made by melting trinitrotoluene (TNT), which melts at a relatively low temperature, and then introducing into the liquid TNT matrix a large fraction of a granular solid explosive such as cyclotrimethylenetrinitramine (RDX) of higher melting temperature which is dispersed and suspended as a particulate solid in the TNT matrix. This mixture can be poured at temperatures above the TNT melting point, and upon cooling the mixture becomes hard. 
     Because of the high cost of TNT, efforts have been and are being made to employ eutectic mixtures of inorganic oxidizers (principally ammonium nitrate) and explosive compounds such as ethylenediaminedinitrate as a replacement for TNT. 
     Both the hard melt-cast composite formulations and the soft emulsion or slurry composite formulations are successful, but each suffers from certain disadvantages. 
     Mixing of molecular explosives is usually accomplished in melt kettles where large quantities of explosives are present in one mass and large distances must separate accumulated quantities of explosives. Of concern are the hazards associated with long dwell times at elevated temperatures because of the increased hazards at higher temperatures. Also troublesome is the shrinkage of these mixtures upon cooling and solidification along with accompanying density gradients, all of which must be accomodated for proper ordnance design. 
     The direction of development of emulsions and slurries has been toward soft or pumpable explosives for commercial blasting operations. Recent developments in such explosive formulations have been water-in-fuel emulsions, having soft or semi-soft consistencies. Patents for such emulsions teach stabilization techniques and fuel-phase continuity. 
     A further development is disclosed in two U.S. Pat. Nos. 4,248,644 and 4,391,659 which teach melt-in-fuel emulsion technology. As taught by these patents, either aqueous salt solutions or essentially anhydrous molten salts can be emulsified with an immiscible hydrocarbon fuel. The hydrocarbon fuel becomes the continuous phase. The discontinuous droplets of oxidizer are very small, and an extremely intimate mixture of fuel and oxidizer is thus obtained. In such oil-continuous emulsions, coalescence and crystallization of the discontinuous droplets of oxidizer may be prevented by making the droplets of oxidizer sufficiently small, and the surface tension such that nucleation may be inhibited; supersaturation or supercooling is achieved, and the emulsion, even though made with molten oxidizer, is formulated to be grease-like or extrudable at ambient temperature. 
     The stabilization of the oil-continuous emulsified state has been a principal objective of recent developments. A soft consistency is desirable for many applications in commercial blasting, and emulsions provide extremely intimate mixtures in a meta-stable state, giving them distinct advantages in explosive sensitivity. Stabilization of the emulsion has been considered desirable since crystallization of the oxidizer salts is accompanied by desensitization of the explosive. In non-aqueous emulsions, sensitivity loss is usually more significant than in aqueous emulsions. Another reason for stabilization of oil-continuous emulsions is to provide and maintain excellent water resistance, as water is effectively kept away from soluble salts by an oil continuum. 
     It has not been apparent heretofore that acceptable, indeed excellent, explosive performance is attainable by deliberate destabilization of an emulsion. It has also not been apparent that excellent water resistance is likewise attainable. In fact, anhydrous, oil-continuous emulsion destabilization has not been disclosed, and thus there is no directly pertinent prior art to this invention. 
     It is the principal objective of this invention to obtain solid, microcrystalline compositions employing essentially anhydrous inorganic oxidizers and hydrocarbon fuels wherein the intimacy of ingredients in the final product is sufficient to obtain excellent explosive and physical characteristics. 
     It is another objective to formulate the compositions in a manner which will permit continuous processing, cooling, optional admixing of additives, and loading or packaging before solidification. 
     Still another objective is to obtain, by extending the range of useable ingredients beyond that which has been applicable to stabilized emulsions or melt-cast explosives, explosive characteristics superior to those which have hitherto been obtained. 
     A further objective is to achieve water resistance in the explosive compositions. 
     SUMMARY OF THE INVENTION 
     This invention describes processes and ingredients by which the above objectives are achieved in explosive compositions, propellants and gas generators. (To avoid redundancy in the discussion which follows, express reference to propellants and gas generators has been limited. However, it is emphasized that the discussion contemplates equally explosives, propellants and gas generators.) This invention effects a new arrangement of matter in which an essentially anhydrous mixture of inorganic oxidizer salts, surfactants and organic fuels is prepared while the oxidizer is molten, and a microcrystalline property is created which imparts a hard, machinable characteristic to the final product. An explosive embodying this invention is called a microknit composite explosive (MCX). 
     It has been found that there are at least three distinctly different processes whereby MCX compositions are attainable. The first method involves dissolving surfactants, crystal habit modifiers, thickeners or combinations into the molten oxidizer. Proper selection and concentration of these ingredients permits supercooling with subsequent solidification resulting in a hard, microcrystalline product. 
     A second method involves the formation of an unstable oil-continuous emulsion as a preliminary step, followed by a controlled disruption of the oil-phase continuum which causes the composition to supercool and then to solidify. In this process a mixture of emulsifier and immiscible oil-like fuel is added to molten oxidizer(s), and an oil-continuous emulsion is formed by mixing. Supercooling is effected by restriction of the size of the oxidizer droplets and their separation from other droplets by the oil-continuous phase. The emulsions, however, are designed to be unstable, i.e., they are deliberately formulated to assure disruption of the oil continuum with subsequent solidification into a hard, microcrystalline product. 
     A third method by which MCX compositions can be made involves salt-continuous emulsions. In these emulsions crystallization normally occurs much more rapidly than in destabilized oil-continuous emulsions. To make the desired MCX compositions by the salt-continuous emulsion route requires that crystal nucleation be retarded by thickeners or crystal habit modifiers or both. By thus retarding crystal nucleation the desired supercooling is achieved with subsequent solidification to a hard product. 
     Each of these methods permits the manufacturing of numerous MCX formulations from separate nonexplosive ingredients. The manufacturing process minimizes both the quantity of neat explosive and residence time at the manufacturing temperature. Safety is greatly enhanced since only small quantities are in process at a given time, which makes practical the use of ingredients which have been hitherto impractical or unsafe. 
    
    
     DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS 
     As examples of the first method described in the summary, several formulations were prepared wherein no immiscible fuel was employed and the desired MCX properties were obtained, namely a hard, microcrystalline product. In the examples cited, a variety of oxidizers was used with several different surfactants, crystal habit modifiers and thickeners. In this process the fuels, solid or liquid, were dissolved into the molten oxidizer. 
     In the first example, Mix 1 in Table I, a mixture of 8 parts sodium dodecylbenzenesulfonate and 4 parts of sodium dimethylnaphthalene (Petro AG) were dissolved into the molten oxidizer at 140° C. The oxidizer was composed of 68.4 parts of NH 4  NO 3  and 9.8 parts each of NaNO 3  and KClO 4 . Both sodium dodecylbenzenesulfonate and Petro AG have a crystal habit modifying and sensitizing effect on NH 4  NO 3 , and they mutually assist in dissolving each other into the oxidizer. Sodium dodecylbenzenesulfonate is a common anionic emulsifier for oil-in-water emulsions. Petro AG is a surfactant, not usually used as an emulsifier. The mix supercooled before solidification, allowing the addition of RDX at temperatures typical of military explosive manufacture. 
     Mix 2 in Table I is a similar NH 4  NO 3  based composition employing a cationic emulsifier of the water-in-oil type, Duomac O. This mix was made by the same procedure used for mix 1, and the desired hard, microcrystalline product was also obtained. 
     Mix 3 in Table I used Duomac O and a crystal habit modifier, hexylaminenitrate. This mix was made in the same manner as mixes 1 and 2 and resulted in the same hard, microcrystalline product. 
     Mix 4 of Table I is a perchlorate based composition employing Duomac O as the only fuel. This mix was made similarly, but at a higher temperature, 180° C. In spite of the higher temperature, this mix supercooled to ambient temperature before solidification to the desired hard, microcrystalline structure. 
     In Table I are several additional compositions wherein the constituents were varied but which resulted in the desired final products. (A key to ingredient abbreviations follows Table I.) 
     
                                           TABLE I__________________________________________________________________________MCX Compositions Made By the First MethodMIX NO.      1  2  3  4   5   6  7__________________________________________________________________________Formulation (wt %)NH.sub.4 NO.sub.3        45.6           66.3              66.3                 --  42.0                         42.0                            67.0NaNO.sub.3   6.5           9.5              9.5                 --  --  -- --KClO.sub.4   6.5           9.5              9.5                 --  20.0                         20.0                            --LiClO.sub.4  -- -- -- 64.0                     --  -- --NH.sub.4 ClO.sub.4        -- -- -- 16.0                     --  -- --Mg(ClO.sub.4).sub.2        -- -- -- --  20.0                         20.0                            20.0SDBS         5.3           -- -- --   2.0                         3.0                            --Duomac O     -- 11.7              7.7                 18.5                     --  6.0                             3.0Petro AG     2.7           -- -- --  --  -- --HAN          -- -- 4.0                 --   4.0                         2.0                            10.0Starch       -- -- -- --  10.0                         -- --Modified Guar        -- -- -- --  --  5.0                            --RDX          33.4           -- -- --  --  -- --Microballoons        -- 3.0              3.0                  1.5                      2.0                         2.0                            --Mfr. temp. (C.)        140°           140°              140°                 180°                     130°                         130°                            120°Test Results @ 10 5° C. in5.0 cm. diameterDensity (g/cc)         1.65            1.15               1.20                  1.50                      1.20                          1.20                             1.60Blasting Cap (#8)        fail           fail              -- --  --  -- fail15 g Tetryl Booster        det           det              det                 det det det                            --__________________________________________________________________________ INGREDIENT KEY TO TABLES SDBS = Sodium dodecylbenzene sulfonate SMO = Sorbitan monooleate HAN = Hexylamine nitrate SLS = Sodium lauryl sulphate Triton X45 = an oxtylphenylethanol, a nonionic surfactant Callimulse = an alkylamine salt of dodecylbenzene sulfonic acid Petro AG = Sodium dimethylnaphthalene sulfonate Terecol 2900 = Polytetrahydrofuran HMT = Hexamethylenetetramine EDD = Ethylenediamine dinitrate MEAP =  Monoethanolamine perchlorate EDNP = Ethylenediamine mononitrate monoperchlorate RDX = Cyclotrimethylenetrinitramine Armac HT = a hydrogenated fatty amine acetate Duomac O = a fatty duomine acetate K.sup.+  Linoleate = potassium linoleate 
    
     As discussed in method two the desired MCX properties can also be obtained using an oil-continuous emulsion as a preliminary step. Examples of MCX explosives made by this method are presented in Table II. In almost all formulations the preliminary emulsions formed either spontaneously or with very little mixing when preheated mixtures of the appropriate surfactants and fuels were added to the molten oxidizer. 
     In all cases the oil-phase continuity of the original emulsion was destroyed to achieve the desired MCX properties. In mixes 1 through 6, emulsions were made to be unstable by the choice of emulsifiers and surfactants employed, thus assuring the destruction of oil-phase continuity and solidification with the desired properties after cooling. Mix 7 was designed originally as a stable emulsion having grease-like consistency at ambient temperature, but to which a surfactant, which is normally used in water-continuous emulsions, was later added in sufficient quantity to destroy the oil-phase continuum. This caused the composition to solidify having MCX properties. The solidified MCX is less sensitive than its precursor emulsion. 
     Note that in mixes 2 and 5 thermoplastic polymers were employed as the fuel. When polymers are used as fuels an elastomeric property is imparted to the product. This elastomeric property is mandatory in many explosive, propellant and gas generator applications. 
     
                                           TABLE II__________________________________________________________________________MCX Compositions Made By The Second Method.Mix No.     1   2     3   4   5    6   7    8__________________________________________________________________________Formulation (wt %)NH.sub.4 NO.sub.3       68.1           73.4  67.2                     --  --   --  61.9 62.1NaNO.sub.3  19.2           --    9.6 --  --   --  --   --LiNO.sub.3  --  --    --  --  --   --  26.0 26.5LiClO.sub.4 --  --    --  58.9                         83.0 44.2                                  --   --KClO.sub.4  --  13.0  9.6 --  --   --  --   --NH.sub.4 ClO.sub.4       --  --    --  24.1                         --   18.1                                  --   --Mg(ClO.sub.4).sub.2       --  --    --  --  --   --  --   --SMO         --  --    --  --  --   --  2.8  2.9Alkatergel  --  --    --  --  --   --  --   --SLS         4.8 --    3.2 --  --   --  --   --Armac HT    --  3.0   --  8.5 --   6.3 --   --Duomac O    --  --    --  --  5.0  --  --   --HAN         --  --    --  --  --   --  2.0  --Mineral oil 4.9 1.0   6.4 --  --   --  6.7  7.0Paraffin wax       --  --    --  8.5 --   6.4 --   --Polythylene --  --    --  --  12.0 --  --   --Terecol 2900       --  6.6   --  --  --   --  --   --Aluminum    --  --    --  --  --   25.0                                  --   --Microballoons       3.0 3.0   4.0 --  --   --  1.5  1.5Mfr. temp. (°C.)       130°           165°                 140°                     185°                         240°                              185°                                  --   90°Results @ 10 5 degrees C.Density (g/cc)        1.10            1.05  1.02                      1.75                          1.40                              2.0  1.30                                        1.30Charge Diameter (cm)       6.3 3.8   6.3 2.5 2.5  2.5 5.0  5.0Blasting Cap (#8)       fail           --    det fail                         det  det det  fail15 g Tetryl Booster       det det   --  --  --   --  --   --Comments:   MCX polymeric                 MCX MCX thermo-                              MCX grease                                       MCX           fuel          plastic  emulsion           MCX           fuel                         MCX__________________________________________________________________________ 
    
     As discussed in method three, the desired MCX properties can also be obtained using salt-continuous emulsions as a preliminary step. In this type of emulsion the desired supercooling may be achieved if the fuels and surfactants allow very fine ingredient intimacy and if the viscosity of the mixture is sufficiently high to retard molecular movement and thus crystal growth. Crystal habit modifiers are also helpful because of their added influence upon nucleation and crystal growth. These emulsions are made in the same manner as in method two, except that higher shear mixing is usually required. Examples of explosives made by this method are presented in Table III. 
     Note that various types of surfactants and thickeners are applicable. Various oxidizer systems and fuels are also useable, with typical MCX physical and explosive properties resulting. Mix 1 illustrates that excellent water resistance is attainable, even without an oil continuum. Table III also shows that explosives can be formulated by this method to have elastomeric physical properties by using elastomers as the principal fuels. 
     
                                           TABLE III__________________________________________________________________________MCX Compositions Made By The Third MethodMix No.        1  2  3  4  5  6  7  8  9__________________________________________________________________________Formulations (wt %)NH.sub.4 NO.sub.3          68.6             68.6                -- 59.0                      59.0                         52.0                            58.3                               58.0                                  50.0NaNO.sub.3     9.8             9.8                -- -- -- -- -- -- --KClO.sub.4     9.8             9.8                -- -- -- -- -- -- 10.0LiClO.sub.4    -- -- 55.3                   -- -- -- -- -- --NH.sub.4 ClO.sub.4          -- -- 23.8                   -- -- -- -- -- --Mg(ClO.sub.4).sub.2          -- -- -- 29.0                      29.0                         26.0                            28.7                               30.0                                  24.0SMO            2.0             -- -- 1.0                      -- -- -- 2.0                                  --SDBS           1.5             2.9                2.0                   -- -- 2.0                            2.0                               1.0                                  --Duomac O       -- 1.0                2.0                   2.0                      -- 2.0                            -- -- --Petro AG       1.5             2.0                1.0                   -- -- -- -- 2.0                                  5.0Hexylamine-    -- -- 2.0                   3.0                      -- 1.0                            -- -- --nitrateTriton X-45    -- -- -- -- 8.0                         -- 2.0                               2.0                                  --Mineral oil    4.8             -- -- 6.0                      -- 2.0                            -- 1.5                                  --Coal tar naphtha          -- 4.9                -- -- 4.0                         -- 1.0                               2.5                                  5.0Styrene        -- -- -- -- -- -- 7.0                               -- --polyesterPolyglycol wax -- -- 12.9                   -- -- -- -- -- --Starch         -- -- -- -- -- 4.0                            -- -- --Silca gel      -- -- -- -- -- -- -- -- 5.0Aluminum       -- -- -- -- -- 10.0                            -- -- --Microballoons  2.0             1.0                1.0                   -- -- 1.0                            1.0                               1.0                                  1.0Mfr. temp. (°C.)Test results @ 10 5 degrees C.in 6.3 cm dia.Density (g/cc)  1.20              1.40                 1.60                    1.65                       1.65                          1.50                             1.40                                1.40                                   1.40#8 cap         fail             -- -- -- -- -- -- -- --15 g Booster   det             fail                det                   fail                      fail                         det                            det                               det                                  det__________________________________________________________________________ 
    
     It has been shown that the desired physical and explosive properties are attainable by different methods, and that one of the desired properties is supercooling before solidification. A broad range of ingredients has also been shown to be applicable in contrast to the narrower range applicable to stabilized oil-continuous emulsions and melt-cast explosives. 
     Broadening the scope of applicable ingredients has many important ramifications. The surface chemistry requirements are much less stringent if the emulsion does not have to be stabilized. Ingredients or manufacturing conditions which interfere with stabilized emulsions can often be used to advantage in MCX formulations. This applies to ingredients in either phase of the original emulsion or to ingredients added after the emulsion is formed. 
     MCX formulations may involve molten oxidizers having melting temperatures considerably in excess of those considered practical for oil-continuous stabilized emulsions. In general, the higher the melting point of the oxidizer, the more difficult it is to stabilize an emulsion. MCX process methodology has been developed for manufacturing at high temperatures with safety, and it has been found practical to make MCX products involving oxidizers having melt temperatures as high as 250° C. Nevertheless, supercooling characteristics have been achieved which allow cooling to ambient or near ambient temperatures before solidification. The use of more powerful oxidizers having higher melting points than those suitable for use in stable oil-continuous emulsions or melt-cast prior art permits the achievement of superior explosive properties in MCX compositions. Mix 1 in Table IV demonstrated cap sensitivity at a density of 2.1 g/cc in a 2.5 cm diameter charge. This was achieved with no self-explosive ingredients or density control agents. 
     MCX formulations also lend themselves to the use of an extended range of fuels including thermoplastic polymers, crosslinkable polymers, and polymerizable fuels. Refinement of the emulsion is critical to stabilize an emulsion, but it is less critical if a stable emulsion is not the aim. Thus higher viscosity fuels are easier to employ in MCX compositions. Further, the use of higher temperatures generally reduces viscosity. For polymerizable or crosslinkable fuels, the chemistry of polymerization or crosslinking has fewer restrictions if emulsion stabilization is not a major concern. A much wider variety of polymeric fuels thus becomes useable. MCX formulations which make use of polymeric fuels are especially applicable to rocket propellants and gas generators wherein resiliency is required. Polyethylene, polystyrene esters, and crosslinkable polyols are examples of polymeric materials which have been successfully employed in MCX formulations, some of which are illustrated in Table IV. 
     
                                           TABLE IV__________________________________________________________________________Miscellaneous MCX FormulationsMix No.     1  2   3   4   5   6   7   8__________________________________________________________________________Formulation (wt %)NH.sub.4 ClO.sub.4       18.1          83.0              --  --  --  --  --  --LiClO.sub.4 44.1          --  60.0                  65.0                      --  --  --  60.0KClO.sub.4  -- --  --  --  --  --  10.0                                  --Mg(ClO.sub.4).sub.2       -- --  --  --  --  --  18.0                                  --NH.sub.4 NO.sub.3       -- --  20.0                  --  --  --  60.0                                  --LiNO.sub.3  -- --  --  --  --  --  --  --NaNO.sub.3  -- --  --  --  --  --  --  --KNO.sub.3   -- --  --  --  --  --  --  --Ca(NO.sub.3).sub.2       -- --  --  --  --  36.6                              --  --LiClO.sub.3 -- --  --  --  84.0                          --  --  --NaClO.sub.3 -- --  --  20.0                      --  47.4                              --  --KNO.sub.2   -- --  --  --  --  --  --  --K.sup.+  Linoleate       -- --  --  --  --  --  --  --SDBC        -- --  --  --  --  --   2.0                                  --SLS         -- --   5.0                  --  --  --  --  --Armac HT     6.4          --  --   7.0                       8.0                          --  --  --Duomac O    --  5.0              --  --  --  12.0                              --   3.0Callimulse  -- --  --  --  --  --  --  --SMO         -- --  --  --  --  --  --  --Petro AG    -- --  --  --  --  --   2.0                                  --HAN         -- --   5.0                  --  --  --  --  --Triton X-45 -- --  --  --  --  --  --  --Stearyl amine       -- --  --  --  --   3.0                              --  --Mineral oil -- --  --  --   8.0                          --  --  --Paraffin wax        6.4          --  --   8.0                      --  --  --   7.0Polythylene -- 12.0              --  --  --  --  --  --Coal tar naphtha       -- --   5.0                  --  --  --   6.0                                  --Terecol 2900       -- --  --  --  --  --  --  --Poly SH     -- --  --  --  --  --  --  --UREA        -- --   5.0                  --  --  --  --  --HMT         -- --  --  --  --  --  --  --EDN         -- --  --  --  --  --  --  --MEAP        -- --  --  --  --  --  --  30.0EDNP        -- --  --  --  --  --  --  --NH.sub.4 ClO.sub.4       -- --  --  --  --  --  --  --Aluminum    25.0          --  --  --  --  --  --  --RDX         -- --  --  --  --  --  --  --Microballoons       -- --  --  --  --   1.0                               2.0                                  --Manufacturing       190°          250°              160°                  170°                      130°                          140°                              125°                                  125°temperature (°C.)Manufacturing        2  2   3   2   2   1   3   2methodResults @ 10 5 deg. C.Density (g/cc)        2.1           1.40               1.80                   1.80                       1.70                           1.60                               1.25                                   1.60Charge Diameter (cm)        2.5           2.5               2.5                   2.5                       2.5                           3.8                               6.3                                   3.8Blasting Cap (#8)       det          det fail                  det det det fail                                  det15 g Tetryl Booster       -- --  --  --  --  --  det --__________________________________________________________________________ 
    
     The range of fuels is extended in other ways. Immiscible fuels having relatively low boiling points (high vapor pressures) are applicable to MCX products but not to oil-continuous emulsions. Fuel vapor pressure is one cause of emulsion breakdown, particularly at high temperatures. In MCX formulations a wider variety of aromatic or aliphatic oils is therefore applicable. A broader spectrum of higher energy fuels and potential sensitizers thus becomes useable. Fuels having high vapor pressures have been employed as emulsion destabilizers in MCX formulations. However, if such fuels are used, it has been found that crystal habit modifiers and rapid cooling are useful to avoid excessive desensitization and ingredient separation. Rapid product cooling provides a large solid surface area upon which the fuels may be adsorbed, thus reducing the opportunity for ingredient separation. 
     The range of polar fuels, those soluble in molten salt, is also extended because such fuels may affect the surface chemistry in a manner disruptive of emulsion stability. 
     Thus, by each of the three methods described, it is possible to produce MCX compositions in which an extremely broad range of ingredients is applicable. Therefore, a correspondingly broad range of claims relating to ingredients is a necessary consequence.