US3883378A - Thermally stable nitrostarch - Google Patents
Thermally stable nitrostarch Download PDFInfo
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- US3883378A US3883378A US596737A US59673766A US3883378A US 3883378 A US3883378 A US 3883378A US 596737 A US596737 A US 596737A US 59673766 A US59673766 A US 59673766A US 3883378 A US3883378 A US 3883378A
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- Prior art keywords
- nitrostarch
- diisocyanate
- complex
- munitions
- thermal stability
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/04—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
- C06B45/06—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
- C06B45/10—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin
- C06B45/105—The resin being a polymer bearing energetic groups or containing a soluble organic explosive
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/04—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
- C06B45/06—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
- C06B45/10—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08B—POLYSACCHARIDES; DERIVATIVES THEREOF
- C08B31/00—Preparation of derivatives of starch
- C08B31/003—Crosslinking of starch
- C08B31/006—Crosslinking of derivatives of starch
Definitions
- a urethane complex consisting of the reaction [52] U.S. Cl 149/108; 260/235 product of nitrostarch and an isocyanate selected from [51] Int. Cl C06b 9/04 the group consisting of [58] Field of Search 149/108, 58, 19; 260/235; 2,4-tolylene diisocyanate,
- nitrocellulose The only high energy polymeric binder currently being employed in conventional propellants is nitrocellulose.
- the attractiveness of nitrocellulose for use in propellants is based on favorable physical characteristics, chemical and thermal stability, and thermochemical properties.
- the physical characteristics of nitrocellulose are such that it can be gclatinized with common solvents to form reasonably tough colloids, which is a necessary characteristic of binders for propellants.
- nitrocellulose is chemically and thermally stable at normal to somewhat higher than normal temperatures.
- nitrocellulose is oxygen sufficient and has a heat of explosion of 940 to 1,140 calories per gram depending upon the nitrogen content. As a result of these features, nitrocellulose has been found to be quite acceptable for use in munitions.
- nitrostarch most nearly exhibits properties comparable to nitrocellulose and may be manufactured at low cost from cheap available material.
- nitrostarch is a mixture of nitrates obtained from nitrating conventional starch, of which sources are practically unlimited. For instance, such starch may be produced from corn, cassava and potatoes which are abundant.
- nitrostarch is considerably less stable than nitrocellulose. For instance, nitrocellulose does not deflagrate after 5 hours exposure at 134.5C whereas nitrostarch deflagrates in 65 minutes at 120 C. As such, nitrostarch in the past has been unacceptable as a substitute for nitrocellulose in munitions.
- Another object is to provide a thermally stable form of nitrostarch, which is a substantial equivalent for nitrocellulose, as a binder for use in propellants.
- a further object is to provide a chemically modified form of nitrostarch having physical, chemical and thermal properties which render it effective as a binder for propellants.
- nitrostarch may be reacted with 2,4-tolylene diisocyanate to form a highly stable form of nitrostarch with respect to its thermal EXAMPLE I
- 34 grams of dry nitrostarch are dissolved in 500 cc of acetone and 1.7 grams of 2,4-tolylene diisocyanate are added.
- the mass is intimately mixed. left standing for about 15 hours, and the resulting lacquer is then added dropwise to water accompanied by vigorous agitation.
- Sufficient water should be used so as not to permit resolvation of the precipated product. For instance,
- EXAMPLE II A dried specimen of approximately 2.5 grams of each of the materials to be tested is placed into an individual test tube and pressed to within 2 inches of the bottom of the tube. Drying of the sample may be initially accomplished on paper trays at a temperature between 38C to 42C. A piece of standardized methyl violet indicator paper is then placed in a vertical position in the tube such that the lower end of the indicator paper is 25mm from the specimen. A cork having a small hole is placed in each tube and the corked tubes are placed in a constant temperature reflux bath at the temperature specified. The tubes are checked at 5 minute intervals to ascertain if there has been any change in the character of the contents.
- Table 1 sets forth the properties of nitrostarch, which has been modified in accordance with this invention, in comparison with those of a nitrostarch control, a nitrocellulose control, and nitrostarch which has been modified with two conventional but entirely different organic stabilizers.
- the nitrostarch control (2) is highly unstable when compared to the nitrocellulose control (1). In fact, at the temperature tested, the nitrocellulose control is at least 5 to times more stable than the nitrostarch control. However, the sample of nitrostarch (3) which has been modified in accordance with this invention is at least 8 to times more stable than the nitrostarch control and is at least as stable as the nitrocellulose control.
- uct is decreased.
- concentration of about 4 to 8% of diisocyanate the procedure produces a product which exhibits the best degree of properties with respect to thermal stability and energy.
- aromatic isocyanates may be utilized in the procedure including such materials as 4,4-diphenylmethane diisocyanate; 1,5-napthalene diisocyanate; p-tolylene isocyanate; 3,3-dimethyl 4,4- biphenyl diisocyanate, phenylene diisocyanate, and 3,3-dimethoxy 4,4'-biphenyl diisocyanate.
- aliphatic isocyanates with carbons ranging from C to C may be employed to stabilize nitrostarch including hexamethylene diisocyanate and heptamethylene diisocyanate.
- a urethane complex consisting of the reaction product of nitrostarch and an isocyanate selected from the group consisting of 2,4-tolylene diisocyanate,
- heptamethylene diisocyanate said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and 2,4-tolylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and 4,4'-diphenylmethane diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and 1.5-napthalene diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and p-tolylene isocyanate. said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and 3,3-dimethoxy 4,4- biphenyl diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and 3,3-dimethyl 4,4- biphenyl diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and phenylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and hexamethylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
- a urethane complex consisting of the reaction product of nitrostarch and heptamethylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
Abstract
1. A urethane complex consisting of the reaction product of nitrostarch and an isocyanate selected from the group consisting of 2,4-TOLYLENE DIISOCYANATE, 4,4''-DIPHENYLMETHANE DIISOCYANATE, 1,5-NAPTHALENE DIISOCYANATE, P-TOLYLENE ISOCYANATE, 3,3''-DIMETHOXY-4,4''-BIPHENYL DIISOCYANATE, 3,3''-DIMETHYL-4,4''-BIPHENYL DIISOCYANATE, PHENYLENE DIISOCYANATE HEXAMETHYLENE DIISOCYANATE, AND HEPTAMETHYLENE DIISOCYANATE, SAID COMPLEX HAVING THERMAL STABILITY ABOVE 65*C for use in munitions.
Description
O United States Patent 1 1 1111 3,883,378
Stack May 13, 1975 [54] THERMALLY STABLE NITROSTARCH 3,157,025 11/1964 Herring et al 149/19 X 3,245,849 4/1966 Kl tal. 149 19 [75] Inventor: Joseph Stack, Rwerdale- 3,256,214 6/1966 13135:? 149/19 [73] Assignee: The United States of America as represented by the Secretary of the Primary Examinew-Stephen J. Lechert, Jr. Army, Washington, DC. Attorney, Agent, or Firm-Nathan Edelberg; Robert P. Filed: Nov- 1966 Glbson; A. V1ctor Erkkila 1 1 pp 596,737 EXEMPLARY CLAIM 1. A urethane complex consisting of the reaction [52] U.S. Cl 149/108; 260/235 product of nitrostarch and an isocyanate selected from [51] Int. Cl C06b 9/04 the group consisting of [58] Field of Search 149/108, 58, 19; 260/235; 2,4-tolylene diisocyanate,
23/75 4,4-diphenylmethane diisocyanate,
1,5-napthalene diisocyanate, [56] References Cited p-tolylene isocyanate,
UNITED STATES PATENTS 3,3-dimeth0Xy-4,4'-bipheny1 diisocyanate, 3,050,423 8/1962 Hudson 149/19 313 l' 'bphenyl dmocyanate 3086.895 4/1963 Schaeffer et a1 149/19 Phenylene dIISOCYEmate 3,092,527 6/1963 Schaafsma 149 19 heXamethylene q p y t and 3,109,761 11/1963 Cobb et a1. 149/19 heptamethylene dusocyanate, 17-893 1/1964 Hedrick et 149/l9 said complex having thermal stability above 65C for 3,131,100 4/1964 Ratliff et a1 149/19 use in munitions 3,132,976 5/1964 Klager et al. 149/19 3,145,192 8/1964 Perry et al 149/19 X 12 Claims, No Drawings 1 THERMALLY STABLE NITROSTARCH This invention relates to a modified form of nitrostarch having improved properties with respect to thermal stability.
The only high energy polymeric binder currently being employed in conventional propellants is nitrocellulose. The attractiveness of nitrocellulose for use in propellants is based on favorable physical characteristics, chemical and thermal stability, and thermochemical properties. The physical characteristics of nitrocellulose are such that it can be gclatinized with common solvents to form reasonably tough colloids, which is a necessary characteristic of binders for propellants. Further, nitrocellulose is chemically and thermally stable at normal to somewhat higher than normal temperatures. Also, nitrocellulose is oxygen sufficient and has a heat of explosion of 940 to 1,140 calories per gram depending upon the nitrogen content. As a result of these features, nitrocellulose has been found to be quite acceptable for use in munitions. However, on the other hand, it is quite advisable for the government to have a broad base of acceptable substitutes for the proven and accepted ingredients of todays munitions such as the conventional binder specified above and the like. But, to date, all efforts to find a polymeric binder for propellants with chemical, physical, thermal and thermo-chemical properties equivalent to nitrocellulose, which is also capable of being produced from cheap available starting material at a low cost, have been unsuccessful.
To date, of all known potential high energy polymeric binder material, nitrostarch most nearly exhibits properties comparable to nitrocellulose and may be manufactured at low cost from cheap available material. As is well known, nitrostarch is a mixture of nitrates obtained from nitrating conventional starch, of which sources are practically unlimited. For instance, such starch may be produced from corn, cassava and potatoes which are abundant. However, one of the major disadvantages of nitrostarch which prohibits its use as an explosive ingredient and potential binder in propellants is its relatively low thermal stability. It is common knowledge that nitrostarch is considerably less stable than nitrocellulose. For instance, nitrocellulose does not deflagrate after 5 hours exposure at 134.5C whereas nitrostarch deflagrates in 65 minutes at 120 C. As such, nitrostarch in the past has been unacceptable as a substitute for nitrocellulose in munitions.
It is therefore an object of this invention to provide an acceptable substitute for nitrocellulose as a binder in propellants.
Another object is to provide a thermally stable form of nitrostarch, which is a substantial equivalent for nitrocellulose, as a binder for use in propellants.
A further object is to provide a chemically modified form of nitrostarch having physical, chemical and thermal properties which render it effective as a binder for propellants.
Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood from the following detailed description.
It has now been discovered that nitrostarch may be reacted with 2,4-tolylene diisocyanate to form a highly stable form of nitrostarch with respect to its thermal EXAMPLE I 34 grams of dry nitrostarch are dissolved in 500 cc of acetone and 1.7 grams of 2,4-tolylene diisocyanate are added. The mass is intimately mixed. left standing for about 15 hours, and the resulting lacquer is then added dropwise to water accompanied by vigorous agitation. Sufficient water should be used so as not to permit resolvation of the precipated product. For instance,
500 cc of the lacquer solution are dropped into 2 liters of water. The precipitate which is formed is then filtered and dried at ambient temperature.
The example which follows illustrates the method of testing the material under study in order to specify the initial, intermediate, and final stages of thermal decomposition of the products set forth in Table 1 below.
EXAMPLE II A dried specimen of approximately 2.5 grams of each of the materials to be tested is placed into an individual test tube and pressed to within 2 inches of the bottom of the tube. Drying of the sample may be initially accomplished on paper trays at a temperature between 38C to 42C. A piece of standardized methyl violet indicator paper is then placed in a vertical position in the tube such that the lower end of the indicator paper is 25mm from the specimen. A cork having a small hole is placed in each tube and the corked tubes are placed in a constant temperature reflux bath at the temperature specified. The tubes are checked at 5 minute intervals to ascertain if there has been any change in the character of the contents.
When the methyl violet indicator paper takes on a salmon pink appearance, the initial degradation of the material is taking place. When red fumes become visually evident, this indicates the visible formation of the oxides of nitrogen, which is the next stage in the degradation of the material under test. In sequence, the material should then explode indicating the time of complete decomposition of the material under study. This latter action is usually accompanied by an audible noise and/or flame.
Table 1 below sets forth the properties of nitrostarch, which has been modified in accordance with this invention, in comparison with those of a nitrostarch control, a nitrocellulose control, and nitrostarch which has been modified with two conventional but entirely different organic stabilizers.
TABLE I Conventionally Conventionally Control Control Stabilized Stabilized Nitrocellulose Nitmstareh Nitrostarch Nitrostarch Nitrostarch Test (12.671N) (12.9471N) (12.55'71N) (12.9471N) (12.9471N) 120C Heat Test, min.
Salmon Pink 90 165 40 85 Red Fumes l None Explosion or Deflagration 300+ 65 500+ 180 210 134.5C Heat Test, min.
Salmon Pink 30-35 45 30 40 Red Fumes 35 8O 30 45 Explosion or Deflagration 300+ 500+ 65 60 Heat of Explosion, cal/g 936 1015 917 Est. 1000 Est. 1000 Effect of Solvents Acetone Colloids Colloids Colloids Colloids Colloids Ether/Alcohol Colloids Colloids Colloids Colloids Colloids As shown, the nitrostarch control (2) is highly unstable when compared to the nitrocellulose control (1). In fact, at the temperature tested, the nitrocellulose control is at least 5 to times more stable than the nitrostarch control. However, the sample of nitrostarch (3) which has been modified in accordance with this invention is at least 8 to times more stable than the nitrostarch control and is at least as stable as the nitrocellulose control. This is clearly an achievement in view of the art which is exemplified by columns 4 and 5 wherein the conventionally modified starches are slightly more stable than the nitrostarch control and less stable than the nitrocellulose control. The nitrostarch of column 4 was modified with resorcinol and the nitrostarch of column 5 was modified with 2-nitrodiphenylamine. These modifiers are known in the art to be conventional stabilizers. Also, as indicated, the nitrostarch modified in accordance with this invention forms a colloid with the conventional solvents which is a prerequisite for its use as a binder in propellants. Further, as a follow-up to Table I, Table 11 below illustrates the range of concentration of 2,4-tolylene diisocyanate that may be used to treat the nitrostarch and the effect of change of concentration on the stability of the modified nitrostarch.
TABLE II 134.5C Heat Test, min. A* Salmon Pink Red Fumes Explosion or Deflagration A percent by weight ol'thc isocyanate compound utilized to treat the nitrostarch.
uct is decreased. At a concentration of about 4 to 8% of diisocyanate, the procedure produces a product which exhibits the best degree of properties with respect to thermal stability and energy.
Although the procedure is described with particular reference to 2,4-tolylene diisocyanate, there are many other types of isocyanate which may be used to treat nitrostarch with comparable results to that shown in Tables I and II. For instance, aromatic isocyanates may be utilized in the procedure including such materials as 4,4-diphenylmethane diisocyanate; 1,5-napthalene diisocyanate; p-tolylene isocyanate; 3,3-dimethyl 4,4- biphenyl diisocyanate, phenylene diisocyanate, and 3,3-dimethoxy 4,4'-biphenyl diisocyanate. These all will react with the available hydroxy groups on the nitrostarch to form a thermally stabilized product which will be acceptable as a substitute for nitrocellulose. In addition, isomers of the above isocyanates may also be effectively used to stabilize nitrostarch. Further, the stability of the nitrostarch, when treated with an aliphatic diisocyanate, would be comparable to that obtained with 2,4-tolylene diisocyanate. In general, aliphatic isocyanates with carbons ranging from C to C may be employed to stabilize nitrostarch including hexamethylene diisocyanate and heptamethylene diisocyanate.
Obviously, many modifications and variations of the present invention are possible in light of the above teaching. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.
I claim:
1. A urethane complex consisting of the reaction product of nitrostarch and an isocyanate selected from the group consisting of 2,4-tolylene diisocyanate,
4,4'-diphenylmethane diisocyanate,
1,5-napthalene diisocyanate,
p-tolylene isocyanate,
3,3' dimethoxy 4,4-biphenyl diisocyanate,
3,3-dimethyl 4,4'-biphenyl diisocyanate,
phenylene diisocyanate hexamethylene diisocyanate, and
heptamethylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
2. The complex of claim 1 wherein said isocyanate is present in an amount between about 1 and percent by weight based on the weight of said nitrostarch.
3. The complex of claim 1 wherein said isocyanate is present in an amount between 4 and 8 percent by weight based on the weight of said nitrostarch.
4. A urethane complex consisting of the reaction product of nitrostarch and 2,4-tolylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
5. A urethane complex consisting of the reaction product of nitrostarch and 4,4'-diphenylmethane diisocyanate, said complex having thermal stability above 65C for use in munitions.
6. A urethane complex consisting of the reaction product of nitrostarch and 1.5-napthalene diisocyanate, said complex having thermal stability above 65C for use in munitions.
7. A urethane complex consisting of the reaction product of nitrostarch and p-tolylene isocyanate. said complex having thermal stability above 65C for use in munitions. I
8. A urethane complex consisting of the reaction product of nitrostarch and 3,3-dimethoxy 4,4- biphenyl diisocyanate, said complex having thermal stability above 65C for use in munitions.
9. A urethane complex consisting of the reaction product of nitrostarch and 3,3-dimethyl 4,4- biphenyl diisocyanate, said complex having thermal stability above 65C for use in munitions.
10. A urethane complex consisting of the reaction product of nitrostarch and phenylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
11. A urethane complex consisting of the reaction product of nitrostarch and hexamethylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
12. A urethane complex consisting of the reaction product of nitrostarch and heptamethylene diisocyanate, said complex having thermal stability above 65C for use in munitions.
Claims (12)
1. A URETHANE COMPLEX CONSISTING OF THE REACTION PRODUCT OF NNITROSTARCHH AND AN ISOCYANATE SELECTED FROM THE GROUP CONSISTING OF 2,4-TOLYLENE DIISOCYANATE, 4,4''-DIPHENYLMETHANE DIISOCYANATE, 1,5-NAPTHALENE DIISOCYANATE, P-TOLYLENE ISOCYANATE, 3,3''-DIMETHOXY - 4,4''-BIPHENYL DIISOCYANATE, 3,3''-DIMETHY - 4,4''-BIPHENYL DIISOCYANATE, PHENYLENE DIISOCYANATE HEXAMETHYLENE DIISOCYANATE, AND HEPTAMETHYLENE DIISOCYANATE, SAID COMPLEX HAVING THERMAL STABILITY ABBOVE 65*C FOR USE IN MUNITIONS.
2. The complex of claim 1 wherein said isocyanate is present in an amount between about 1 and 15 percent by weight based on the weight of said nitrostarch.
3. The complex of claim 1 wherein said isocyanate is present in an amount between 4 and 8 percent by weight based on the weight of said nitrostarch.
4. A urethane complex consisting of the reaction product of nitrostarch and 2,4-tolylene diisocyanate, said complex having thermal stability above 65*C for use in munitions.
5. A urethane complex consisting of the reaction product of nitrostarch and 4,4''-diphenylmethane diisocyanate, said complex having thermal stability above 65*C for use in munitions.
6. A urethane complex consisting of the reaction product of nitrostarch and 1,5-napthalene diisocyanate, said complex having thermal stability above 65*C for use in munitions.
7. A urethane complex consisting of the reaction product of nitrostarch and p-tolylene isocyanate, said complex having thermal stability above 65*C for use in munitions.
8. A urethane complex consisting of the reaction product of nitrostarch and 3,3''-dimethoxy - 4,4''-biphenyl diisocyanate, said complex having thermal stability above 65*C for use in munitions.
9. A urethane complex consisting of the reaction product of nitrostarch and 3,3''-dimethyl - 4,4''-biphenyl diisocyanate, said complex having thermal stability above 65*C for use in munitions.
10. A urethane complex consisting of the reaction product of nitrostarch and phenylene diisocyanate, said complex having thermal stability above 65*C for use in munitions.
11. A urethane complex consisting of the reaction product of nitrostarch and hexamethylene diisocyanate, said complex having thermal stability above 65*C for use in munitions.
12. A urethane complex consisting of the reaction product of nitrostarch and heptamethylene diisocyanate, said complex having thermal stability above 65*C for use in munitions.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US596737A US3883378A (en) | 1966-11-23 | 1966-11-23 | Thermally stable nitrostarch |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US596737A US3883378A (en) | 1966-11-23 | 1966-11-23 | Thermally stable nitrostarch |
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US3883378A true US3883378A (en) | 1975-05-13 |
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US596737A Expired - Lifetime US3883378A (en) | 1966-11-23 | 1966-11-23 | Thermally stable nitrostarch |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4303786A (en) * | 1977-08-04 | 1981-12-01 | Ramot - Tel-Aviv University | Isonitrile derivatives of macromolecules containing hydroxyl groups |
EP0124398A1 (en) * | 1983-03-28 | 1984-11-07 | ETAT-FRANCAIS représenté par le Délégué Général pour l' Armement | Compressed propellant charge for munition and process for its manufacture |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3050423A (en) * | 1959-06-15 | 1962-08-21 | Phillips Petroleum Co | Solid propellant |
US3086895A (en) * | 1958-11-05 | 1963-04-23 | Thiokol Chemical Corp | Solid composite propellant containing acetylenic polyurethane and process of making |
US3092527A (en) * | 1960-10-25 | 1963-06-04 | United Aircraft Corp | Propellant mixing |
US3109761A (en) * | 1958-04-03 | 1963-11-05 | Phillips Petroleum Co | Easily castable polyurethane propellants containing highly halogenated compounds |
US3117898A (en) * | 1958-10-30 | 1964-01-14 | Monsanto Chemicals | Solid propellant containing lithium perchlorate |
US3131100A (en) * | 1957-12-20 | 1964-04-28 | Phillips Petroleum Co | Solid propellants comprising a polyurethane and a copolymer of a conjugated diene |
US3132976A (en) * | 1959-07-20 | 1964-05-12 | Aerojet General Co | Solid propellant compositions containing polyurethane resins |
US3145192A (en) * | 1957-07-01 | 1964-08-18 | Thiokol Chemical Corp | Acetylenic polyurethanes useful as propellants |
US3157025A (en) * | 1959-06-10 | 1964-11-17 | Phillips Petroleum Co | Rocket motor and solid propellant charge |
US3245849A (en) * | 1959-07-20 | 1966-04-12 | Aerojet General Co | Solid propellant compositions containing polyurethane resins of low cure temperature |
US3256214A (en) * | 1962-09-17 | 1966-06-14 | Atlas Chem Ind | Polyurethane resin prepared from an organic polyisocyanate and a nitric acid partial ester of a polyhydroxy compound |
-
1966
- 1966-11-23 US US596737A patent/US3883378A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3145192A (en) * | 1957-07-01 | 1964-08-18 | Thiokol Chemical Corp | Acetylenic polyurethanes useful as propellants |
US3131100A (en) * | 1957-12-20 | 1964-04-28 | Phillips Petroleum Co | Solid propellants comprising a polyurethane and a copolymer of a conjugated diene |
US3109761A (en) * | 1958-04-03 | 1963-11-05 | Phillips Petroleum Co | Easily castable polyurethane propellants containing highly halogenated compounds |
US3117898A (en) * | 1958-10-30 | 1964-01-14 | Monsanto Chemicals | Solid propellant containing lithium perchlorate |
US3086895A (en) * | 1958-11-05 | 1963-04-23 | Thiokol Chemical Corp | Solid composite propellant containing acetylenic polyurethane and process of making |
US3157025A (en) * | 1959-06-10 | 1964-11-17 | Phillips Petroleum Co | Rocket motor and solid propellant charge |
US3050423A (en) * | 1959-06-15 | 1962-08-21 | Phillips Petroleum Co | Solid propellant |
US3132976A (en) * | 1959-07-20 | 1964-05-12 | Aerojet General Co | Solid propellant compositions containing polyurethane resins |
US3245849A (en) * | 1959-07-20 | 1966-04-12 | Aerojet General Co | Solid propellant compositions containing polyurethane resins of low cure temperature |
US3092527A (en) * | 1960-10-25 | 1963-06-04 | United Aircraft Corp | Propellant mixing |
US3256214A (en) * | 1962-09-17 | 1966-06-14 | Atlas Chem Ind | Polyurethane resin prepared from an organic polyisocyanate and a nitric acid partial ester of a polyhydroxy compound |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4303786A (en) * | 1977-08-04 | 1981-12-01 | Ramot - Tel-Aviv University | Isonitrile derivatives of macromolecules containing hydroxyl groups |
EP0124398A1 (en) * | 1983-03-28 | 1984-11-07 | ETAT-FRANCAIS représenté par le Délégué Général pour l' Armement | Compressed propellant charge for munition and process for its manufacture |
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