EP3753916B1 - Composite pyrotechnical product - Google Patents

Description

Field of the invention

The present invention relates to composite pyrotechnic products, suitable in particular as solid propellants for propellant charges of tactical missiles. These composite pyrotechnic products have good mechanical properties when cold and at room temperature.

State of the art

Solid propellants are used for the propulsion of rockets or missiles. Mention may in particular be made in this respect of double-base propellants and composite propellants. A composite-type solid propellant comprises powdery solid fillers (oxidizing fillers, with, possibly in addition, reducing fillers) as well as various additives, in particular feasibility additives and performance additives, in a generally plasticized binder (a polymer matrix solid - a cross-linked polymer - energetic or not, generally plasticized). The binder is typically obtained from a liquid (“crosslinkable”) polymer, having chemically reactive ends, capable of being crosslinked by at least one (at least bifunctional) crosslinking agent which is also liquid. Is in fact generally introduced into such a liquid polymer, in an appropriate order, at least one plasticizer and the other ingredients of the propellant, with the exception of said at least one crosslinking agent (and at least one crosslinking catalyst, if such at least one crosslinking catalyst (generally very sensitive to humidity) is used), then finally said at least one crosslinking agent (and said optional at least one crosslinking catalyst used). The filled polymer is then heat-treated (“baked”) at a temperature compatible with the energetic materials ( minimum fillers) present. The crosslinked polymer constitutes, with the plasticizer(s) present(s), the plasticized binder, which coats all the ingredients and in particular the pulverulent fillers, to finally form a solid body. Solid propellants suitable for rocket motors are described in patent application WO 2016/066945 . Solid propellants suitable for missiles are described in the patent application WO 2018/055312 . Other solid propellants are described in the applications CN-A-107 721 784 , KR-A-2010 0035522 and CN-A-107 879 868 ; in the first two documents, the propellants contain 500 ppm of crosslinking catalyst, whereas in the third document the propellants contain a small quantity (10 to 20% by mass) of energetic charges.

• des performances énergétiques élevées sans particule, à fumée réduite, à température de combustion modérée ;
• des propriétés balistiques adaptées à une large gamme d'applications tactiques ;
• des produits de combustion compatibles avec les concepts avancés (vannage) ;
• un excellent comportement en vieillissement, respectueux de l'environnement, non sensible à l'électricité statique.

The objectives sought for solid propellants are generally the following:

• high energy performance without particles, with reduced smoke, at a moderate combustion temperature;
• ballistic properties suitable for a wide range of tactical applications;
• combustion products compatible with advanced concepts (valving);
• excellent aging behavior, environmentally friendly, not sensitive to static electricity.

The development of new solid propellants requires a fine balance so as not to improve a given property to the detriment of another property. Thus lowering the level of plasticizer in the binder can lead to a drop in energy performance; likewise the choice of the crosslinking agent can have an impact on the energy properties.

The objective of the present invention is to provide composite pyrotechnic products which have good mechanical properties over a wide range of temperatures, and in particular when cold and at room temperature.

Summary of the invention

It has been demonstrated, against all expectations, that it is possible to obtain composite pyrotechnic products having improved mechanical properties, without impacting their energy performance, by increasing the amount of crosslinking catalyst used.

Thus, according to one aspect, the invention relates to a composite pyrotechnic product containing organic energetic charges in a plasticized binder, comprising a crosslinked energetic polymer and at least one energetic plasticizer, said energetic polymer being crosslinked in the presence of 150 to 400 ppm of au least one crosslinking catalyst, the organic energetic charges representing from 50 to 70% by mass of the composition of the composite pyrotechnic product.

According to another aspect, the invention relates to a method for preparing said composite pyrotechnic product.

According to another aspect, the invention relates to the use of said composite pyrotechnic product as solid propellant for a propellant charge of a missile, in particular of a tactical missile.

Brief description of the figure

The figure 1 represents the elongation at break and the mechanical capacity of a composite pyrotechnic product representative of the invention.

Description of the invention

• le polymère énergétique réticulé consiste en un polyazoture de glycidyle (PAG), ayant une masse moléculaire moyenne en nombre (Mn) comprise entre 700 et 3000 g/mol, obtenu par réticulation, via ses fonctions terminales hydroxyles, à l'aide d'au moins un agent de réticulation de type polyisocyanate, en présence d'environ 150 ppm à environ 500 ppm d'au moins un catalyseur de réticulation.

According to one aspect, the present invention relates to new composite pyrotechnic products, having excellent mechanical properties. These composite products are of the cross-linked energetic binder type containing organic energetic fillers. More specifically, the composite products in accordance with the invention contain organic energetic fillers in a plasticized binder, comprising a crosslinked energetic polymer and at least one energetic plasticizer. Characteristically:

• the cross-linked energetic polymer consists of a polyglycidyl azide (PAG), having a number-average molecular mass (Mn) of between 700 and 3000 g/mol, obtained by cross-linking, via its terminal hydroxyl functions, using at at least one crosslinking agent of polyisocyanate type, in the presence of about 150 ppm to about 500 ppm of at least one crosslinking catalyst.

The nature of the binder (that of its precursor polymer (energetic)) constitutes one of the important elements of the invention. The quantity of crosslinking catalyst used constitutes another important element of the invention.

With reference to the nature of the binder (therefore energetic binder), more particularly to that of its precursor polymer (hydroxytelechelic glycidyl polyazide), the following can be added.

It is in no way excluded from the scope of the invention that a mixture of at least two glycidyl polyazides (having molecular masses (between 700 and 3000 g/mol) and/or different branching rates) be used as precursor polymer of the binder of the products of the invention.

The energetic polymer precursor of the binder of the products of the invention is therefore a polyglycidyl azide (PAG) which has terminal hydroxy functions (a hydroxytelechelic PAG), hence 1) its energetic properties and 2) its ability to be crosslinked with polyisocyanate-type crosslinking agents.

Said polymer has an adequate molecular mass (in particular, with reference to its consistency (liquid) and to the consistency of its mixture with essentially the fillers (organic energetics) and with reference to the relative content of the crosslinked binder in crosslinking agent(s) ), number-average molecular weight (Mn) of between 700 and 3000 g/mol, advantageously between 1700 and 2300 g/mol.

Crosslinking agents, of polyisocyanate type (at least bifunctional), suitable for crosslinking such a hydroxytelechelic polyglycidyl azide (PAG) are known per se. They may in particular be di- or triisocyanates. It is advantageously polyisocyanates, liquids, chosen from toluene diisocyanate (TDI), isophorone diisocyanate (IPDI), dicyclohexylmethylene diisocyanate (MDCI), hexamethylene diisocyanate (HDI), the trimer of said hexamethylene diisocyanate (in particular marketed by the company Bayer under the trade name Desmodur® N 3300), biuret ^trihexane isocyanate (BTHI), 3,5,5-trimethyl-1,6-hexamethylene diisocyanate and mixtures thereof. Particularly preferably, the trimer of hexamethylene diisocyanate is used.

Said crosslinking agents are conventionally used in a necessary and sufficient quantity to ensure the crosslinking of the polymer (not excessive so as not to pollute the crosslinked product obtained). They are conventionally used in an amount such that the bridging ratio (NCO (of the crosslinking agent) /OH (of the polymer)) is between approximately 0.8 and approximately 1.4, advantageously between approximately 0.8 and approximately 1.1.

The crosslinked energetic polymer generally represents from 9 to 14% by mass of the total composition of the composite pyrotechnic products of the invention.

It has been clearly understood that the advantage of the invention is based on the level of crosslinking of the binder precursor polymer, energetic, this level resulting from the quantity of crosslinking catalyst used, namely approximately 150 ppm to approximately 400 ppm, advantageously approximately 200ppm to about 400ppm. It will be noted here that the quantity of crosslinking catalyst is expressed relative to the mass of composite pyrotechnic product. The crosslinking catalyst is advantageously chosen from triphenylbismuth (Biφ ₃ ), dibutyltin dilaurate (DBTL), and mixtures thereof. In one embodiment of the invention, the crosslinking catalyst is a mixture of triphenylbismuth and dibutyltin dilaurate, advantageously in a mass ratio ranging from approximately 75:25 to approximately 95:5, for example 75:25, 80 :20, 85:15, 90:10 or 95:5.

Conventionally, the energetic binder is associated with at least one energetic plasticizer. The energetic plasticizer(s) in question is (are) advantageously of the nitrate and/or nitramine type. The energetic plasticizer(s) in question is (are) very advantageously chosen from diethylene glycol dinitrate (DEGDN); triethylene glycol dinitrate (TEGDN); butanetriol trinitrate (BTTN); trimethylolethane trinitrate (TMETN); a mixture of 2,4-dinitro-2,4-diaza-pentane, 2,4-dinitro-2,4-diaza-hexane and 3,5-dinitro-3,5-diaza-heptane (and especially DNDA 5.7); nitrato ethyl nitramines (in particular methyl-2-nitratoethyl nitramine (methylNENA) and ethyl-2-nitratoethyl nitramine (ethylNENA)); and their mixtures.

The plasticizer(s) of the pyrotechnic products of the invention generally represent(s) from 10 to 30% by mass, more generally from 15 to 25% by mass, of the total composition of said products.

The energy charges present are organic charges.

The organic energetic charges in question are not per se original. These are organic energetic fillers known per se and, for the most part, already packaged according to the prior art in crosslinked energetic polymeric binders (in particular of the PAG type). These are advantageously hexogen (RDX), octogen (HMX), hexanitrohexaazaisowurtzitane (CL20), nitroguanidine (NGU), ethylene dinitramine (EDNA), N-guanylurea dinitramide (FOX 12 (GUDN)), 1,1-diamino-2,2-dinitro ethylene (FOX 7 (DADE)), bis(triaminoguanidinium) 5,5'-azotetrazolate (TAGZT), 5,5'-azotetrazolate dihydrazinium (DHDZT), 5,5'-bis(tetrazolyl)hydrazine (HBT), bis(2,2-dinitropropyl) nitramine (BDNPN), a nitropyrazole or a mixture of these fillers (organic energetics ).

Within the composite pyrotechnic products of the invention, there is therefore a type of energetic charge, advantageously chosen from the list above, or a mixture of at least two types of energetic charge, advantageously chosen from the list above. .

Preferably, there are energetic fillers of RDX and/or HMX, more preferably energetic fillers of RDX or HMX.

The use of hexogen fillers and/or octogen fillers is particularly recommended insofar as these two types of fillers offer a very satisfactory compromise: safety/energetic power.

The organic energetic charges are conventionally in the form of solid grains, distributed homogeneously within the plasticized crosslinked binder. These solid grains conveniently present, in a manner known per se, several particle size distributions.

The organic energetic charges of the composite pyrotechnic products of the invention represent from 50 to 70% by mass, generally from 55 to 65% by mass, of the total composition of said products. It has been understood that said products have a high filler content.

It should be noted that the presence of metallic fillers (of aluminium, in particular), within the plasticized binder of the composite pyrotechnic products of the invention, is itself generally excluded. Such metallic charges are indeed likely to generate particles during their combustion, ie to generate primary smoke. The presence of inorganic energetic fillers (of ammonium perchlorate, in particular), within the plasticized binder of the pyrotechnic products of the invention, is not desired but cannot be totally excluded. In any case, such inorganic energetic charges, present, are necessarily present in small quantities (<4% by mass). They can be considered as ballistic additives (see below). Their presence may be appropriate, with reference to the desired ballistic properties of the product.

The composite pyrotechnic products of the invention are moreover capable of containing, and generally contain, in their binder (crosslinked precursor polymer), in addition to the plasticizer(s) and organic energetic fillers, at least one ballistic additive. We can more accurately speak of at least one other ballistic additive, the crosslinking catalyst being able to be analyzed as an additive in its own right. The crosslinking catalysts have been presently isolated from the other additives, insofar as they are present with reference to the technical problem presently considered.

Among the ballistic additives conveniently present, preference is given to the following conventional additives: agents for stabilizing the energetic plasticizer(s) present, ballistic catalysts and anti-glare agents. Thus, according to an advantageous variant, the composite pyrotechnic products of the invention therefore contain in their composition, in addition to the crosslinked polymer (PAG), the plasticizer(s) and the organic energetic fillers, at least one ballistic additive; said at least one ballistic additive comprising at least one agent for stabilizing the plasticizer(s) present and/or at least one ballistic catalyst and/or at least one anti-glare agent. Mention may be made, as stabilizing agent of the plasticizer(s), of aromatic amines, such as in particular 2-nitrodiphenylamine (2-NDPA) and N-methylparanitroaniline (MNA). Present, it is generally present at a content of approximately 1% by mass. By way of ballistic catalyst, mention may be made of conventional ballistic catalysts, such as in particular salts and oxides of lead, and bismuth citrate. Said bismuth citrate, in particular because of its lower toxicity, is preferred. Said at least one ballistic catalyst is generally present in the composition of the pyrotechnic products of the invention at a content of approximately 1% to approximately 6% by mass, very generally at a content of approximately 3% to approximately 5% by mass . As an anti-glare agent, mention may be made of compounds based on alkali metals, sodium (Na ₂ SO ₄ , etc.) and especially potassium (K ₂ SO ₄ , KNO ₃ , K ₃ AlF ₆ , C ₄ H ₅ KO ₆ , etc.). Advantageously, the anti-glare agent is cryolite potassium (= potassium aluminum fluoride; (K ₃ AlF ₆ )), monobasic potassium tartrate (C ₄ H ₅ KO ₆ ) (said monobasic potassium tartrate possibly being in the form of L- enantiomer or D- or in racemic form.These specific potassium salts are commercially available, in conventional particle sizes (powders with grains generally having a d ₅₀ between 1 and 300 µm).Present, the anti-glare agent is generally present at a content of approximately 1% to approximately 5% by weight Other ballistic additives likely to be present in the composition of the composite pyrotechnic products of the invention may in particular consist of inorganic energetic fillers (see above).

The ballistic additives that may be present (in view of the comments above, it has been understood that generally several types of additive are present) generally represent a maximum of approximately 10% by mass of the composition of the composite pyrotechnic products of the invention. They very generally represent approximately 0.1% to approximately 10% by mass (often approximately 1.5% to approximately 10% by mass) of the composition of said composite pyrotechnic products of the invention.

• de environ 50% à environ 70%, avantageusement de environ 55% à environ 65%, de charges énergétiques organiques,
• de environ 9% à environ 4 % de polymère énergétique (de type PAG hydroxytéléchélique) réticulé (via ses fonctions terminales hydroxy par au moins un polyisocyanate),
• de environ 10% à environ 30%, avantageusement de environ 15% à environ 25%, d'au moins un plastifiant énergétique,
• de 0 à environ 10%, avantageusement de environ 0,1% à environ 10%, d'au moins un additif balistique.

In one embodiment, the composition of the composite pyrotechnic products of the invention, expressed in mass percentages, contains:

• from approximately 50% to approximately 70%, advantageously from approximately 55% to approximately 65%, of organic energy charges,
• from approximately 9% to approximately 4% of energetic polymer (of hydroxytelechelic PAG type) crosslinked (via its terminal hydroxy functions by at least one polyisocyanate),
• from approximately 10% to approximately 30%, advantageously from approximately 15% to approximately 25%, of at least one energetic plasticizer,
• from 0 to approximately 10%, advantageously from approximately 0.1% to approximately 10%, of at least one ballistic additive.

It is understood that the advantageous ranges indicated above can entirely be considered independently of each other. Preferably, they are in combination with each other.

In the context of this embodiment, said composition is generally free of any other ingredient (in particular of any metallic filler) and therefore consists of the ingredients listed above, present in the amounts indicated above.

The preparation of the composite pyrotechnic products in accordance with the invention does not pose any particular difficulties. It can in particular be implemented by the method specified below, which constitutes another aspect of the invention. This is a process by analogy, which, characteristically, involves the at least one crosslinking catalyst, in the preparation of a propellant with a binder of the crosslinked hydroxytelechelic PAG type.

• la constitution d'une pâte homogène par
  1. a) incorporation, avec agitation, à une température comprise entre environ 35°C et environ 55°C, dans un polyazoture de glycidyle adéquat (PAG hydroxytéléchélique présentant une masse moléculaire en nombre telle que précisée ci-dessus), d'au moins un plastifiant énergétique, des charges énergétiques organiques et des autres ingrédients constitutifs du produit pyrotechnique composite recherché à l'exception d'un quelconque agent de réticulation et d'un quelconque catalyseur de réticulation, et
  2. b) agitation du mélange résultant, sous vide partiel, à une température comprise entre environ 35°C et environ 55°C ;
• l'incorporation dans ladite pâte homogène constituée, sous vide partiel et à une température comprise entre environ 35°C et environ 55°C, dudit au moins un agent de réticulation et d'environ 150 ppm à environ 400 pm dudit au moins un catalyseur de réticulation, suivie d'une agitation du mélange constitué ;
• la coulée dudit mélange constitué dans au moins une structure ; et
• le traitement thermique dudit mélange constitué agité coulé dans ladite au moins une structure.

The present invention therefore also relates to a method for preparing a composite pyrotechnic product, as described above. This process includes:

• the constitution of a homogeneous paste by
  1. a) incorporation, with stirring, at a temperature of between approximately 35° C. and approximately 55° C., in a suitable glycidyl polyazide (hydroxytelechelic PAG having a molecular mass in number as specified above), of at least one energetic plasticizer, organic energetic fillers and other constituent ingredients of the desired composite pyrotechnic product with the exception of any crosslinking agent and any crosslinking catalyst, and
  2. b) stirring the resulting mixture, under partial vacuum, at a temperature between about 35°C and about 55°C;
• the incorporation into said homogeneous paste formed, under partial vacuum and at a temperature between about 35°C and about 55°C, of said at least one crosslinking agent and of about 150 ppm to about 400 μm of said at least one catalyst crosslinking, followed by stirring of the mixture formed;
• casting said constituted mixture into at least one structure; and
• the heat treatment of said stirred mixture cast in said at least one structure.

The partial vacuum mentioned is intended for the degassing of the medium above which it is applied. It is generally around 10 mm Hg. We note incidentally that it is not necessarily of constant intensity.

The heat treatment (for crosslinking (of the hydroxytelechelic PAG)) is generally carried out at a temperature of between about 30° C. and about 60° C. (30° C.≤T≤60° C.), for several days.

The composite pyrotechnic products in accordance with the invention are particularly suitable as solid propellants for propellant charges for missiles, in particular tactical missiles. Their use for this purpose is particularly recommended. It forms an integral part of the present invention.

• ils possèdent d'excellentes propriétés mécaniques à froid et à température ambiante, sans baisse de performance énergétique ;
• ils peuvent être fabriqués de manière satisfaisante et compatible avec une montée en maturité à échelle industrielle.

The composite pyrotechnic products in accordance with the invention have in particular the following advantages:

• they have excellent mechanical properties when cold and at room temperature, with no drop in energy performance;
• they can be manufactured satisfactorily and compatible with an increase in maturity on an industrial scale.

The invention will be better understood using the examples below, given purely by way of illustration.

Example 1

Into a mixer, hydroxytelechelic glycidyl polyazide (PAG) (marketed by the company EURENCO (Mn=1900 g/mol) was introduced, then plasticizers (BTTN/TMETN, mixture 30/70 by mass), stabilizing agents (MNA /2-NDPA, mixture 75/25 by weight) of said plasticizers and ballistic additives. The mixture was mixed for 15 min at a temperature of 40° C. The organic energy charges (mixture by mass of 2/3 RDX 0-100 and 1/3 RDX M3C) per portion, then the ballistic catalyst (bismuth citrate) in portions Stirring was then continued for 2h30, still at a temperature of 40° C and under a vacuum of 10 mm Hg (which allowed degassing of the medium), to obtain a homogeneous paste. The crosslinking catalyst (20 ppm DBTL + 200 ppm Biφ ₃ ) was then added to said homogeneous paste and the medium was further stirred 30 min before the addition of the crosslinking agent of the binder (trimer of hexamethylene diisocyanate sold by Bayer under the trade name Desmodur ^® N 3300). The medium was further stirred for 15 min (still at 40° C. and under vacuum). 2 kg of propellant paste were thus obtained, the composition of which is indicated in Table 1. A sample was taken from each of the propellant pastes thus prepared for the determination of the pot life. The rest of the propellant paste was then cast in a suitable structure and then subjected to heat treatment (baking at a temperature of 50° C. for 14 days).

Comparative example

The procedure of example 1 was repeated but using as crosslinking catalyst a mixture of 5 ppm of DBTL and 50 ppm of Biφ ₃ . The composition of the propellant paste obtained is shown in Table 1. Table 1 Compound (% mass) Ex.1 e.g. comp PAG 9.0 9.0 BTTN/TMETN 20.2 20.2 MNA/2-NDPA 0.7 0.7 RDX 61.5 61.5 Bi-citrate 4 4 DBTL 20ppm 5ppm Biφ ₃ 200ppm 50ppm Ballistic additives 2.6 2.5 ^Desmodur® N 3300 2.0 2.1

Example 2

The pot life (which makes it possible to assess the feasibility of the propellant production process) was determined by measuring the viscosity of the propellant paste in question (containing the crosslinking agent and the crosslinking catalyst) at over time, using a Brookfield viscometer (with body No. 3 (mobile C) rotated at 1 revolution/min), at a temperature of 40°C. The time for which the viscosity reached 1500 Pa.s was recorded, in order to determine whether the propellant met the industrialization criterion, that is to say whether said recorded time was greater than 10 h. The results are shown in Table 2. Table 2 Ex.1 e.g. comp potty life > 8 p.m. ≈ 70h

Example 3

The various mechanical properties of the propellant blocks obtained according to the above examples were evaluated over a wide temperature range: modulus of elasticity (E), stress (Sm), elongation at break (em) and mechanical capacity (shown by the product Sm ^∗ em) as a function of t/a _τ (time-temperature equivalence). The measurements were taken by uniaxial traction in accordance with the NFT70-315 standard.

The results are presented in Table 3 below and on the figure 1 . Table 3 Ex.1 e.g. comp + 20°C 50 mm/min E (Mpa) 8.8 4.1 Sm (Mpa) 0.74 0.50 em (%) 42 40 Sm/E 0.08 0.12 Sm∗em 31 20 -20°C 50mm/min E (Mpa) 13.0 7.2 Sm (Mpa) 0.99 0.73 em (%) 36 33 Sm/E 0.08 0.12 Sm∗em 36 24 -20°C 500mm/min E (Mpa) 21.6 14.2 Sm (Mpa) 1.45 1.37 em (%) 40 33 Sm/E 0.07 0.10 Sm∗em 58 45 -46°C 500mm/min E (Mpa) 869 342 Sm (Mpa) 11.4 11.6 em (%) 8 6 Sm/E 0.01 0.03 Sm∗em 91 64

It can be seen from reading the table above that a significant increase in the quantity of crosslinking catalyst during the preparation of the propellant paste (x4) results in a significant increase in the stress Sm and the modulus E at +20°C for a tensile speed of 50 mm/min without degrading the elongation em. The mechanical capacity is therefore significantly improved. When cold (-20°C at 5 mm/min and -20°C at 500 mm/min), the observed effect is even more interesting: the increase in stress and modulus is combined with that of elongation . The figure 1 shows the order of magnitude of the gains in elongation and mechanical capacity for the different conditions tested.

Claims (13)

1. A composite pyrotechnic product containing organic energetic charges in a plasticized binder, comprising a cross-linked energetic polymer and at least one energetic plasticizer, said cross-linked energetic polymer consisting of a polyglycidyl azide (PGA), having a number-average molecular weight (Mn) of between 700 and 3000 g/mol, obtained by crosslinking, via its hydroxyl terminal functions, with at least one crosslinking agent of polyisocyanate type, in the presence of 150 ppm to 400 ppm of at least one crosslinking catalyst, the organic energetic charges representing from 50 to 70% by weight of the composition of the composite pyrotechnic product.
2. The composite pyrotechnic product of claim 1, wherein the polyglycidyl azide (PGA) has a number molecular weight (Mn) of between 1700 and 2300 g/mol.
3. The composite pyrotechnic of claim 1 or claim 2, wherein said at least one energetic plasticizer is of the nitrate and/or nitramine type.
4. The composite pyrotechnic product of any one of claims 1 to 3, wherein said organic energetic charges are selected from hexogen charges, octogen charges, and mixtures of such charges.
5. The composite pyrotechnic product of any one of claims 1 to 4, wherein the cross-linking catalyst is selected from tin dibutyldilaurate, triphenylbismuth, and mixtures thereof.
6. The pyrotechnic product of claim 5, wherein the cross-linking catalyst is a mixture of triphenylbismuth and tin dibutyldilaurate.
7. The composite pyrotechnic of any one of claims 1 to 6, wherein the amount of cross-linking catalyst is from 200 ppm to 400 ppm.
8. The composite pyrotechnic of any one of claims 1 to 7, which further comprises at least one ballistic additive.
9. The composite pyrotechnic product of claim 8, wherein said at least one ballistic additive is selected from an energetic plasticizer(s) stabilizing agent, a ballistic catalyst and mixtures thereof.
10. The composite pyrotechnic product of claim 8 or claim 9, which contains bismuth citrate as a ballistic catalyst.
11. The composite pyrotechnic product of any one of claims 1 to 10, the composition of which, expressed as percentages by weight, contains :

    - from 50 to 70%, advantageously from 55 to 65%, of organic energetic charges,

    - from 9 to 14% of cross-linked energetic polymer,

    - from 10 to 30%, advantageously from 15 to 25%, of energetic plasticizer(s),

    - from 0 to 10%, advantageously from 0.1 to 10%, of at least one ballistic additive.
12. Use of the composite pyrotechnic product of any one of claims 1 to 11, as a solid propellant of a propellant charge of a missile, in particular of a tactical missile.
13. A method of preparing a composite pyrotechnic of any one of claims 1 to 11, which comprises:

    - forming a homogeneous paste by

    a) incorporating, at a temperature comprised between 35°C and 55°C, into said polyglycidyl azide, said at least one energetic plasticizer, the organic energetic charges and the other constituent ingredients of the desired composite pyrotechnic product with the exception of any cross-linking agent and any cross-linking catalyst, and

    b) stirring the resulting mixture, under partial vacuum, at a temperature comprised between 35°C and 55°C;

    - incorporating in said homogeneous constituted paste, under partial vacuum and at a temperature comprised between 35°C and 55°C, said at least one cross-linking agent and at least one cross-linking catalyst, followed by stirring the constituted mixture;

    - casting said stirred constituted mixture into at least one structure; and

    - heat-treating said stirred constituted mixture cast into said at least one structure.

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