US3794535A - Pyrotechnic lacquer - Google Patents

Pyrotechnic lacquer Download PDF

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US3794535A
US3794535A US00271803A US3794535DA US3794535A US 3794535 A US3794535 A US 3794535A US 00271803 A US00271803 A US 00271803A US 3794535D A US3794535D A US 3794535DA US 3794535 A US3794535 A US 3794535A
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pyrotechnic
lacquer
collodion
propellant
powders
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Y Bertrand
R Grebert
J Paquet
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Societe Nationale des Poudres et Explosifs
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Societe Nationale des Poudres et Explosifs
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    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C7/00Non-electric detonators; Blasting caps; Primers
    • C06C7/02Manufacture; Packing
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/18Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
    • C06B25/24Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with nitroglycerine
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00Compositions containing a nitrated organic compound
    • C06B25/18Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
    • C06B25/24Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with nitroglycerine
    • C06B25/26Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition with nitroglycerine with an organic non-explosive or an organic non-thermic component
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B33/00Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • C06B33/12Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide the material being two or more oxygen-yielding compounds
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones

Definitions

  • the pyrotechnic compositions may be alumino-thermal powders, therrntes, black powders or zirconium/barium chromate/ammonium perchlorate/ammonium bichromate, and the collodion may be a nitrocellulose or nitroglycerine powders (or mixtures of the two), or a plastics material, in solution in solvent.
  • the present invention relates to a pyrotechnic lacquer used especially for producing ignition compositions for blocks of solid propellant and charges for gas generators.
  • a lacquer which comprises a dispersion of: (a) a pyrotechnic composition in a tinely divided form, chosen from the group comprising aluminothermal powders (a mixture of potassium perchlorate and aluminium powder), ⁇ flo-called thermite powders (a mixture of potassium perchlorate, iron oxide and magnesium), black powder and powders based on zirconium, barium chromate, ammonium perchlorate or ammonium bichromate, in (b) a collodion containing either a powder based on nitrocellulose, on plasticized nitricellulose or on a mixture of nitrocellulose and nitroglycerine, dissolved in a volatile solvent for the said powder, especially a ketone solvent such as acetone or methyl ethyl ketone, or a plastics material dissolved in an organic solvent, especially polyethylene dissolved in trichloroethylene, polyvinyl chloride dissolved in methyl e
  • the proportions in which the pyrotechnic composition and the collodion are used are from 5 to 99.5%, preferably from 40 to 60%, by weight for the former and from 95 to 0.5% and preferably 60 to 40%, by weight of the latter.
  • the collodion preferably contains 75% by weight of powder or of plastics material and 25% of solvent.
  • the pyrotechnic composition should preferably have a particle size of less than 500 microns.
  • the pyrotechnic lacquer of the invention is especially useful as an ignition composition for blocks of solid propellant.
  • That face of the block to be ignited is coated with a layer of the pyrotechnic lacquer and the solvent is evaporated.
  • the ignition composition thus obtained can advantageously replace the conventional triggering box containing black powder, which is usually fixed by glue to a face of the propellant block and which can become detached and thereby cause spoilage of the guide system during ignition.
  • the pyrotechnic lacquer according to the invention can also be used to produce pyrotechnic charges for gas generators of the type described in our French patent applications Nos. /44,837 and 70/44,838.
  • the outer wall of the vaporizable liquid chamber of the gas generator is coated, partially or completely, with the pyrotechnic lacquer of the invention and the solvent is evaporated from the layer of lacquer.
  • FIG. l is a cross-section in side elevation of a block of propellant provided with a layer of a lacquer of the invention
  • PIG. 2 is a front elevation of the same block
  • FIGS. 3 and 4 are graphs illustrating the results of experiments carried out in vacuo on the pyrotechnic lacquer and on the propellant:
  • FIGS. 5 and 6 are graphs illustrating the ignition phase of tirings of the blocks of propellant of Examples 2 and 3, respectively.
  • EXAMPLE 1 Preparation of the pyrotechnic composition 45 parts by weight of zirconium, 34 parts of barium chromate, 14 parts of ammonium perchlorate and 7 parts of ammonium bichromate were mixed together by means of a Moritz mixer running at low speed, for one hour.
  • GB Tu powder a powder based on nitrocellulose and on nitroglycerine, in the ratio of 58:42, containing 1.1% of centralite as a stabilizer
  • Preparation of the pyrotechnic lacquer 60 parts by weight of the pyrotechnic composition were mixed with 40 parts of collodion. Mixing was carried out in a climatically controlled area at 2l-29 C. and 30- 40% relative humidity.
  • the pyrotechnical lacquer thus obtained was used to produce, by coating, an ignition composition on a block of Epictte propellant plasticized nitrocellulose and njtroglycerine) for frontal combustion, of which a crosssection in side elevation is shown in FIG. l of the accompanying drawing, and a front elevation in FIG. 2.
  • This cylindrical block l diameter 78 mm., was perforated by an axial cylindrical channel 2, 1.5 mm. in diameter, and was covered with a layer of inhibitor 3 on its side wall, in the said channel and on its front face.
  • the rear face 1a of this block was coated with a layer 4 of the pyrotechnic lacquer prepared above, 5 g. of this lacquer being uniformly spread over a ring of external diameter 60 mm. and internal diameter l0 mm.
  • the layer of lacquer was thereafter dried in a climatically controlled area at 21-29 C. and at 30-40% relative humidity for several hours in order to produce, on this block of propellant, a layer of ignition composition of about 1 mm. thickness.
  • Vacuum test This test was carried out at temperature of 90 C., 100 C. and 110 C.
  • test sample for a test at a given temperature, was l g.
  • Vacuum test-test on the pyrotechnic lacquer In view of the high sensitivity of the composition to mechanical pyrotechnic factors, this test was carried out on a dry mixture of 2 parts of the said pyrotechnic composition and of 3 parts of finely ground collodion slab.
  • the study was based on ageing for two to six months at 60 C.
  • the tests were carried out on four cubes of 25 mm. side length, of which one face was entirely coated with pyrotechnic lacquer to a thickness equivalent to that produced on the block of propellant.
  • a test cycle comprised:
  • EXAMPLE 2 A pyrotechnic lacquer was prepared by mixing 40 parts by weight of a thermite powder of the following composition:
  • the graph in FIG. 5 shows the pressure in bars (as the ordinate) as a function of the period of combustion in seconds (as the abscissa), illustrating the ignition phase of a tiring using the block of propellant which was ignited by means of the pyrotechnic lacquer of this example, applied by coating.
  • EXAMPLE 3 A pyrotechnic lacquer was prepared by mixing 40 parts by weight of blackpower with 60 parts of collodion of the type described in Example 1.
  • the graph in FIG. 6 shows the pressure in bars (as the ordinate) as a function of the period of combustion in seconds (as the abscissa), illustrating the ignition phase of a firing using the block of propellant which was ignited by means of the pyrotechnic lacquer of this example, applied.
  • EXAMPLE 4 A pyrotechnic lacquer was prepared by mixing 2 parts by weight of a thermite powder having the following composition:
  • This lacquer was directly coated onto the outer wall of the vaporizable liquid chamber of the gas generator described in Belgian Pats. 775,997 and 775,422, both granted Dec. l5, 1971, to which correspond U.S. applications, Ser. No. 206,662 and Ser. No. 205,046, and was dried in a climatically controlled area at 2129 C. and at 30-40% relative humidity for several hours so as to yield a 2.25 mm. layer of a gas generator composition, as a replace ment of the charge of propellant in hollow strands, with which the said gas generator was equipped.
  • a lacquer which comprises a dispersion of: (a) a pyrotechnic composition in finely divided form, selected from the group consisting of powders consisting of (l) ferrie oxide, magnesium and potassium perchlorate, (2) of black powder and (3) of powders consisting of zirconium, barium chromate, ammonium perchlorate and ammonium bichromate. in (b) a collodion which consists of a powder based on nitrocellulose and nitroglycerine cerine dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition, and from 60-40% by weight of said collodion.
  • a lacquer according to claim 1 which comprises a dispersion of 3 parts by weight of a pyrotechnic composition consisting of zirconium, barium chromate, ammonium perchlorate and ammoium bichromate in the respective proportion 45:34: 14:7, in 2 parts by weight of a collodion consisting of 75% of a power based on nitrocellulose and nitroglycerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
  • a pyrotechnic composition consisting of zirconium, barium chromate, ammonium perchlorate and ammoium bichromate in the respective proportion 45:34: 14:7
  • a collodion consisting of 75% of a power based on nitrocellulose and nitroglycerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
  • a lacquer according to claim 1 which comprises a dispersion of 2 parts by weight of a pyrotechnic composition consisting of FegOs, Mg and KCIO4 in the respective proportions 34:36:30 in 3 parts by weight of a collodion consisting of 75% of a powdei based on nitrocellulose and nitroglyoerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
  • a lacquer according to claim 1 which comprises a dispersion of 2 parts by weight of a pyrotechnic composition consisting of black powder in 3 parts by weight of a collodion consisting of 75% of powder based on nitrocellulose and nitroglycerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
  • a solid propellant grain having an ignition face coated with a layer of a lacquer which comprises a dispersion of: (a) a pyrotechnic composition, in finely divided form, selected from the group consisting of (1) powders consisting of ferrie oxide, magnesium and potassium perchlorate, (2) black powder and (3) powders consisting of zirconium, barium chromate, ammonium perchlorate and ammonium bichromate in (b) a collodion which consists of a powder based on mixtures of nitrocellulose and nitroglycerine, said powder being dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition and from 6() to 40% by weight of said collodion.
  • a pyrotechnic composition in finely divided form, selected from the group consisting of (1) powders consisting of ferrie oxide, magnesium and potassium perchlorate, (2) black powder and (3) powders consisting of zirconium, barium chromate,
  • a charge for a gas generator comprising a vaporizable liquid chamber having an outer wall, said charge consisting of a layer of lacquer coating said outer wall, said lacquer comprising a dispersion of: (a) a pyrotechnic composition, in nely divided form, selected from the group consisting of powders consisting of ferrie oxide, magnesium and potassium perchlorate, black powder and powders based on zirconium, barium chromate, ammonium perchlorate and ammonium bichromate in (b) a collodion which consists of a powder based on mixtures of nitrocellulose and nitroglycerine, said powder being dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition and from 60 to 40% by weight of collodion.
  • a pyrotechnic composition in nely divided form, selected from the group consisting of powders consisting of ferrie oxide, magnesium and potassium perchlorate
  • solvent is selected from acetone and methyl ethyl ketone. 15 149-8, 12, 38, 40, 42, 44, 65, 73, 76, 85

Abstract

LACQUERS COMPRISING A DISPERSION OF A PYROTECHNIC COMPOSITION IN A COLLODION, WHICH ARE USEFUL IN FORMING IGNITION COATINGS ON BLOCKS OF PROPELLANT AND GAS GENERATORS, THE PYROTECHNIC COMPOSITIONS MAY BE ALUMINO-THERMAL POWDERS, THERMITES, BLACK POWDERS OR ZIRCONIUM/BARIUM CHROMATE/AMMONIUM PERCHLORATE/AMMONIUM BICHROMATE, AND THE COLLODION MAY BE A NITROCELLULOSE OR NITROGLYCERINE POWDERS (OR MIXTURES OF THE TWO), OR A PLASTICS MATERIAL, IN SOLUTION IN SOLVENT.

Description

Feb- 26. 1974 Y. H. BERTRAND ETAL PYROTBCHNIC LACQUER Filed July 14, 1972 3 Sheets-Sheet l Feb. 26, 1974 Y. BERTRAND ETAL 3,794,535
PYROTECHNIC LACQUER 5 Sheets-Sheet 2 Filed July 14, 1972 fur-4 Feb. 26, 1974 Y H BERTRAND ETAL 3,794,535
PYROTECHN I C LACQUER Filed July 14, 1972 3 Sheets-Sheet a 3 01.6 9 liz 1,'5 1,18 2i. I4 7 3.10Y
United States Patent Office Patented Feb. 26, 1974 U.S. Cl. 149-3 7 Claims ABSTRACT F THE DISCLOSURE Lacquers comprising a dispersion of a pyrotechnic composition in a collodion, which are useful in forming ignition coatings on blocks of propellant and gas generators. The pyrotechnic compositions may be alumino-thermal powders, therrntes, black powders or zirconium/barium chromate/ammonium perchlorate/ammonium bichromate, and the collodion may be a nitrocellulose or nitroglycerine powders (or mixtures of the two), or a plastics material, in solution in solvent.
The present invention relates to a pyrotechnic lacquer used especially for producing ignition compositions for blocks of solid propellant and charges for gas generators.
According to the invention, there is provided a lacquer which comprises a dispersion of: (a) a pyrotechnic composition in a tinely divided form, chosen from the group comprising aluminothermal powders (a mixture of potassium perchlorate and aluminium powder), `flo-called thermite powders (a mixture of potassium perchlorate, iron oxide and magnesium), black powder and powders based on zirconium, barium chromate, ammonium perchlorate or ammonium bichromate, in (b) a collodion containing either a powder based on nitrocellulose, on plasticized nitricellulose or on a mixture of nitrocellulose and nitroglycerine, dissolved in a volatile solvent for the said powder, especially a ketone solvent such as acetone or methyl ethyl ketone, or a plastics material dissolved in an organic solvent, especially polyethylene dissolved in trichloroethylene, polyvinyl chloride dissolved in methyl ethyl ketone or a cellulosic polymer dissolved in ethyl acetate.
The proportions in which the pyrotechnic composition and the collodion are used are from 5 to 99.5%, preferably from 40 to 60%, by weight for the former and from 95 to 0.5% and preferably 60 to 40%, by weight of the latter. Furthermore, the collodion preferably contains 75% by weight of powder or of plastics material and 25% of solvent.
Additionally, the pyrotechnic composition should preferably have a particle size of less than 500 microns.
The pyrotechnic lacquer of the invention is especially useful as an ignition composition for blocks of solid propellant. For this purpose, that face of the block to be ignited is coated with a layer of the pyrotechnic lacquer and the solvent is evaporated. The ignition composition thus obtained can advantageously replace the conventional triggering box containing black powder, which is usually fixed by glue to a face of the propellant block and which can become detached and thereby cause spoilage of the guide system during ignition.
The pyrotechnic lacquer according to the invention can also be used to produce pyrotechnic charges for gas generators of the type described in our French patent applications Nos. /44,837 and 70/44,838. For this purpose, the outer wall of the vaporizable liquid chamber of the gas generator is coated, partially or completely, with the pyrotechnic lacquer of the invention and the solvent is evaporated from the layer of lacquer.
The pyrotechnic lacquers of the invention have numerous advantages:
they do not require baking and polymerization operations; they are stable on storage in a leakproof container; and their speed of combustion can easily be varied by varying the charge content or by changing the nature of the collodion or the nature of the pyrotechnic composition.
In order that the invention may be more fully understood, the following examples are given by way of illustration only. In addition, reference is made to the accompanyng drawings, in which:
FIG. l is a cross-section in side elevation of a block of propellant provided with a layer of a lacquer of the invention;
PIG. 2 is a front elevation of the same block;
FIGS. 3 and 4 are graphs illustrating the results of experiments carried out in vacuo on the pyrotechnic lacquer and on the propellant: and
FIGS. 5 and 6 are graphs illustrating the ignition phase of tirings of the blocks of propellant of Examples 2 and 3, respectively.
EXAMPLE 1 Preparation of the pyrotechnic composition 45 parts by weight of zirconium, 34 parts of barium chromate, 14 parts of ammonium perchlorate and 7 parts of ammonium bichromate were mixed together by means of a Moritz mixer running at low speed, for one hour.
Preparation of the collodion parts by weight of GB Tu powder (a powder based on nitrocellulose and on nitroglycerine, in the ratio of 58:42, containing 1.1% of centralite as a stabilizer) were dissolved in 25 parts of acetone.
Preparation of the pyrotechnic lacquer 60 parts by weight of the pyrotechnic composition were mixed with 40 parts of collodion. Mixing was carried out in a climatically controlled area at 2l-29 C. and 30- 40% relative humidity.
The pyrotechnical lacquer thus obtained was used to produce, by coating, an ignition composition on a block of Epictte propellant plasticized nitrocellulose and njtroglycerine) for frontal combustion, of which a crosssection in side elevation is shown in FIG. l of the accompanying drawing, and a front elevation in FIG. 2.
This cylindrical block l, diameter 78 mm., was perforated by an axial cylindrical channel 2, 1.5 mm. in diameter, and was covered with a layer of inhibitor 3 on its side wall, in the said channel and on its front face.
The rear face 1a of this block was coated with a layer 4 of the pyrotechnic lacquer prepared above, 5 g. of this lacquer being uniformly spread over a ring of external diameter 60 mm. and internal diameter l0 mm.
The layer of lacquer was thereafter dried in a climatically controlled area at 21-29 C. and at 30-40% relative humidity for several hours in order to produce, on this block of propellant, a layer of ignition composition of about 1 mm. thickness.
The compatability of the pyrotechnic lacquer with the propellant was demonstrated by the following tests:
Vacuum test This test was carried out at temperature of 90 C., 100 C. and 110 C.
The test sample, for a test at a given temperature, was l g.
Vacuum test-test on the pyrotechnic lacquer In view of the high sensitivity of the composition to mechanical pyrotechnic factors, this test was carried out on a dry mixture of 2 parts of the said pyrotechnic composition and of 3 parts of finely ground collodion slab.
The results shown on the graph of FIG. 3 give, the pressure loss in mm. (as the ordinate) as a function of the time in days (as the abscissa).
Vacuum test"-on chips of propellent The results are shown on the graph of FIG. 4.
superposition of the graphs of FIGS. 3 and 4 shows an identical behaviour of the propellant and of the pyrotechnic composition/collodion" mixture in the experiments of the vacuum test.
Furthermore, the resistance to ageing of the ignition composition obtained from the pyrotechnic lacquer was demonstrated by the so-called test cube test.
The study was based on ageing for two to six months at 60 C. The tests were carried out on four cubes of 25 mm. side length, of which one face was entirely coated with pyrotechnic lacquer to a thickness equivalent to that produced on the block of propellant.
A test cycle comprised:
(a) 18 hours temperatuure exposure in an oven thermostated to :L- l.50 C. and
(b) Removal from the oven for 6 hours, during which a visual and radiographic check of the propellant-ignition composition interface was made on each cube.
The results obtained after 22 cycles at 60 C. were that, at 60 C., no detachment of the ignition composition, and no cracking in the propellant, was observed.
EXAMPLE 2 A pyrotechnic lacquer was prepared by mixing 40 parts by weight of a thermite powder of the following composition:
Percent Fe203 34 Mg 36 KC104 30 with 60 parts of collodion of the type described in Example l.
The face of a Butalpite block of propellant (polybutadiene-potassium perchlorate) which was to be ignited, of diameter 94 mm., was coated with 5 g. of this lacquer.
The graph in FIG. 5 shows the pressure in bars (as the ordinate) as a function of the period of combustion in seconds (as the abscissa), illustrating the ignition phase of a tiring using the block of propellant which was ignited by means of the pyrotechnic lacquer of this example, applied by coating.
EXAMPLE 3 A pyrotechnic lacquer was prepared by mixing 40 parts by weight of blackpower with 60 parts of collodion of the type described in Example 1.
The face of a homogenous block of powder (nitrocellulose-nitroglycerine), 33 mm. in diameter, was coated with 5 g. of this lacquer.
The graph in FIG. 6 shows the pressure in bars (as the ordinate) as a function of the period of combustion in seconds (as the abscissa), illustrating the ignition phase of a firing using the block of propellant which was ignited by means of the pyrotechnic lacquer of this example, applied.
EXAMPLE 4 A pyrotechnic lacquer was prepared by mixing 2 parts by weight of a thermite powder having the following composition:
Percent Fe203 34 Mg 36 KClO4 30 with 3 parts by weight of a collodion of the type described in Example I.
This lacquer was directly coated onto the outer wall of the vaporizable liquid chamber of the gas generator described in Belgian Pats. 775,997 and 775,422, both granted Dec. l5, 1971, to which correspond U.S. applications, Ser. No. 206,662 and Ser. No. 205,046, and was dried in a climatically controlled area at 2129 C. and at 30-40% relative humidity for several hours so as to yield a 2.25 mm. layer of a gas generator composition, as a replace ment of the charge of propellant in hollow strands, with which the said gas generator was equipped.
We claim:
1. A lacquer which comprises a dispersion of: (a) a pyrotechnic composition in finely divided form, selected from the group consisting of powders consisting of (l) ferrie oxide, magnesium and potassium perchlorate, (2) of black powder and (3) of powders consisting of zirconium, barium chromate, ammonium perchlorate and ammonium bichromate. in (b) a collodion which consists of a powder based on nitrocellulose and nitroglycerine cerine dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition, and from 60-40% by weight of said collodion.
2. A lacquer according to claim 1 which comprises a dispersion of 3 parts by weight of a pyrotechnic composition consisting of zirconium, barium chromate, ammonium perchlorate and ammoium bichromate in the respective proportion 45:34: 14:7, in 2 parts by weight of a collodion consisting of 75% of a power based on nitrocellulose and nitroglycerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
3. A lacquer according to claim 1, which comprises a dispersion of 2 parts by weight of a pyrotechnic composition consisting of FegOs, Mg and KCIO4 in the respective proportions 34:36:30 in 3 parts by weight of a collodion consisting of 75% of a powdei based on nitrocellulose and nitroglyoerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
4. A lacquer according to claim 1, which comprises a dispersion of 2 parts by weight of a pyrotechnic composition consisting of black powder in 3 parts by weight of a collodion consisting of 75% of powder based on nitrocellulose and nitroglycerine in the respective proportions of 58 to 42 and containing 1.1% of centralite and 25% of acetone.
5. A solid propellant grain having an ignition face coated with a layer of a lacquer which comprises a dispersion of: (a) a pyrotechnic composition, in finely divided form, selected from the group consisting of (1) powders consisting of ferrie oxide, magnesium and potassium perchlorate, (2) black powder and (3) powders consisting of zirconium, barium chromate, ammonium perchlorate and ammonium bichromate in (b) a collodion which consists of a powder based on mixtures of nitrocellulose and nitroglycerine, said powder being dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition and from 6() to 40% by weight of said collodion.
6. A charge for a gas generator comprising a vaporizable liquid chamber having an outer wall, said charge consisting of a layer of lacquer coating said outer wall, said lacquer comprising a dispersion of: (a) a pyrotechnic composition, in nely divided form, selected from the group consisting of powders consisting of ferrie oxide, magnesium and potassium perchlorate, black powder and powders based on zirconium, barium chromate, ammonium perchlorate and ammonium bichromate in (b) a collodion which consists of a powder based on mixtures of nitrocellulose and nitroglycerine, said powder being dissolved in a ketonic solvent, the dispersion containing from 40 to 60% by weight of the pyrotechnic composition and from 60 to 40% by weight of collodion.
7. A lacquer according to claim 1 wherein the ketonic References Cited UNITED STATES PATENTS ONeill et al. 149--96 X Ryker et al 149-96 X ONeill 149-96 X Vandersmith et al. 149-10 X Coffee 149-96 X Herzog et al 149-96 X Hamilton 149-8 X STEPHEN I. LECHERT, JR., Primary Examiner U.S. CI. X.R.
solvent is selected from acetone and methyl ethyl ketone. 15 149-8, 12, 38, 40, 42, 44, 65, 73, 76, 85
US00271803A 1971-07-19 1972-07-14 Pyrotechnic lacquer Expired - Lifetime US3794535A (en)

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AU (1) AU464153B2 (en)
BE (1) BE786494A (en)
BR (1) BR7204788D0 (en)
CA (1) CA987911A (en)
DK (1) DK130662B (en)
ES (1) ES404944A1 (en)
FR (1) FR2146555A5 (en)
GB (1) GB1378789A (en)
IE (1) IE36547B1 (en)
IT (1) IT964715B (en)
LU (1) LU65710A1 (en)
NL (1) NL7209998A (en)
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4084078A (en) * 1977-02-15 1978-04-11 American Service Products, Inc. Jet perforator device
US4339288A (en) * 1978-05-16 1982-07-13 Peter Stang Gas generating composition
US4390380A (en) * 1980-03-31 1983-06-28 Camp Albert T Coated azide gas generating composition
US6077372A (en) * 1999-02-02 2000-06-20 Autoliv Development Ab Ignition enhanced gas generant and method
US6165296A (en) * 1999-02-02 2000-12-26 Autoliv Development As Gas generant igniter composition and method
US20030217666A1 (en) * 2002-05-21 2003-11-27 Trw Airbag Systems Gmbh Tubular gas generator
US20050123406A1 (en) * 2003-12-05 2005-06-09 Marcus Clark Inflator devices having a moisture barrier member
ITMC20090251A1 (en) * 2009-12-15 2011-06-16 Blasio Elio Di PETARDO WITH TRIGGERING PASTRY ACTIVATED WITH FLAME ALIVE OR INCANDESCENT AND RELATIVE PRODUCTION METHOD.
US20150099102A1 (en) * 2013-10-08 2015-04-09 Lawrence Livermore National Security, Llc Multifunctional reactive inks, methods of use and manufacture thereof
US20190301842A1 (en) * 2018-03-30 2019-10-03 Beau Waswo Gun Disabling Mock Ammunition

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2626875B1 (en) * 1975-12-17 1991-11-08 Onera (Off Nat Aerospatiale) IMPROVEMENTS IN IGNITION MEANS FOR FUEL GAS GENERATORS WITH SOLID REACTIVE MASS
FR2624113B1 (en) * 1987-12-03 1990-04-20 France Etat EJECTION CHARGE FOR CLOSE DEFENSE AMMUNITION
FR2638451B1 (en) * 1988-11-03 1993-12-03 Ruggieri METHOD FOR PRODUCING A FIRE TRANSMISSION CONDUIT AND CONDUIT OBTAINED BY THIS METHOD
GB9119217D0 (en) * 1991-09-09 1991-10-23 Ici Plc Low energy fuse
GB2267330A (en) * 1992-05-23 1993-12-01 Secr Defence Laser ignition of gas generators
RU2492159C1 (en) * 2012-05-21 2013-09-10 Открытое акционерное общество Федеральный научно-производственный центр "Научно-исследовательский институт прикладной химии" Incendiary pyrotechnic composition for bengal candles

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4084078A (en) * 1977-02-15 1978-04-11 American Service Products, Inc. Jet perforator device
US4339288A (en) * 1978-05-16 1982-07-13 Peter Stang Gas generating composition
US4390380A (en) * 1980-03-31 1983-06-28 Camp Albert T Coated azide gas generating composition
US6077372A (en) * 1999-02-02 2000-06-20 Autoliv Development Ab Ignition enhanced gas generant and method
US6165296A (en) * 1999-02-02 2000-12-26 Autoliv Development As Gas generant igniter composition and method
US6834594B2 (en) * 2002-05-21 2004-12-28 Trw Airbag Systems Gmbh & Co. Kg Tubular gas generator
US20030217666A1 (en) * 2002-05-21 2003-11-27 Trw Airbag Systems Gmbh Tubular gas generator
US20050123406A1 (en) * 2003-12-05 2005-06-09 Marcus Clark Inflator devices having a moisture barrier member
US7185588B2 (en) 2003-12-05 2007-03-06 Autoliv Asp, Inc. Inflator devices having a moisture barrier member
ITMC20090251A1 (en) * 2009-12-15 2011-06-16 Blasio Elio Di PETARDO WITH TRIGGERING PASTRY ACTIVATED WITH FLAME ALIVE OR INCANDESCENT AND RELATIVE PRODUCTION METHOD.
US20150099102A1 (en) * 2013-10-08 2015-04-09 Lawrence Livermore National Security, Llc Multifunctional reactive inks, methods of use and manufacture thereof
US10377090B2 (en) * 2013-10-08 2019-08-13 Lawrence Livermore National Security, Llc Multifunctional reactive inks, methods of use and manufacture thereof
US11370927B2 (en) * 2013-10-08 2022-06-28 Lawrence Livermore National Security, Llc Multifunctional reactive inks, methods of use and manufacture thereof
US20190301842A1 (en) * 2018-03-30 2019-10-03 Beau Waswo Gun Disabling Mock Ammunition
US11187501B2 (en) * 2018-03-30 2021-11-30 Beau Waswo Gun disabling mock ammunition

Also Published As

Publication number Publication date
ES404944A1 (en) 1975-07-16
SE437149B (en) 1985-02-11
BR7204788D0 (en) 1973-12-18
AU4459572A (en) 1974-01-17
ZA724771B (en) 1973-04-25
IE36547L (en) 1973-01-19
LU65710A1 (en) 1974-01-21
BE786494A (en) 1973-01-19
FR2146555A5 (en) 1973-03-02
AR193278A1 (en) 1973-04-11
GB1378789A (en) 1974-12-27
DE2234264B2 (en) 1975-10-16
CA987911A (en) 1976-04-27
DK130662B (en) 1975-03-17
DE2234264A1 (en) 1973-01-25
IT964715B (en) 1974-01-31
AU464153B2 (en) 1975-08-14
NO130006B (en) 1974-06-24
IE36547B1 (en) 1976-11-24
NL7209998A (en) 1973-01-23
DK130662C (en) 1975-08-25

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