WO1998021168A1 - Agent propulsif contenant un elastomere thermoplastique a haute energie - Google Patents
Agent propulsif contenant un elastomere thermoplastique a haute energie Download PDFInfo
- Publication number
- WO1998021168A1 WO1998021168A1 PCT/US1996/018372 US9618372W WO9821168A1 WO 1998021168 A1 WO1998021168 A1 WO 1998021168A1 US 9618372 W US9618372 W US 9618372W WO 9821168 A1 WO9821168 A1 WO 9821168A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- propellant
- percent
- high energy
- thermoplastic elastomer
- oxetane
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B25/00—Compositions containing a nitrated organic compound
- C06B25/34—Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
-
- 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
Definitions
- the present invention relates generally to a ihigh energy propellant composition. More particularly the invention relates to a propellant that includes an energetic thermoplastic elastomer as a binder and a high energy, high density filler. I ,
- one object of the present invention is to provide a pair of high energy propellants whose average impetus is at or above the 1300 J/g level.
- Another object of this invention is to provide a pair of high energy propellants whose burning rate differential is three or greater.
- An additional object of this invention is to provide new energetic materials and processes that eliminate or greatly reduce both volatile organic compound production and ancillary waste through demil and recyclability.
- TNAZ Trimethylolethane Trinitrate or TMETN
- Triethylene Glycol Dinitrate or TEGDN Bis, 2,2 - Dinitro propyl acetal/Bis 2,2 - Diniro propyl formal or BDNPA/F
- Methyl Nitrato ethyl nitramine or methyl NENA ethyl NENA.
- plasticizers may be used alone or in combination.
- a pair of high energy propellants may be combined to produce a propellant mixture having a first propellant having a burning rate at least three times faster than the burning rate of the second propellant.
- the first propellant includes an oxetane thermoplastic elastomer energetic binder admixed with CL-20 high energy explosive filler.
- the second propellant including an oxetane thermoplastic
- the ratio of burning rates may I be varied from at least 2.0 times to as high as 4.8 times, or higher ⁇
- plasticizers and relative amounts for each of the first and second propellants are within the same ranges as for the single propellants.
- steps of mixing at about 95 °C and extruding at slightly lower temperatures Processing at these temperatures provided a safe operating margin of at least 50 ° C because the self heat temperatures of the filler ranges from about 175 °C to 192 °C, but the preferred plasticizer TNAZ melts around 100 °C, so that as some of the TNAZ begins to melt during processing at 95 °C, a more fluid mix results that is easier to process.
- Table II seven formulations that have been prepared. All values for the composition are given in percent by weight, based on the total weight. !
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Dispersion Chemistry (AREA)
- Molecular Biology (AREA)
- Crystallography & Structural Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
Agent propulsif à haute énergie contenant un liant énergétique élastomère thermoplastique d'oxétane, mélangé à une charge explosive à haute énergie. Le liant énergétique élastomère thermoplastique d'oxétane constitue, de préférence, environ 5 à 30 % en poids de la composition et la charge explosive à haute énergie constitue environ 70 à 95 % en poids de la composition. Un agent propulsif préféré comprend également un plastifiant explosif, de préférence à raison d'environ 4 à 7 %. La charge préférée est choisie dans le groupe constitué de CL-20, TNAZ, RDX et de mélanges de ceux-ci. Le plastifiant préféré est choisi dans le groupe constitué de TNAZ, BTTN, TMETN, TEGDN, BDNPA/F, NENA méthylique, NENA éthylique et des mélanges de ceux-ci. Dans un mode de réalisation préféré, l'agent propulsif est constitué de deux agents propulsifs à haute énergie, comprenant un mélange d'un premier et d'un second agent propulsif à haute énergie, le premier agent ayant une vitesse de combustion au moins deux fois supérieure à celle du second agent. Le premier agent propulsif comporte un liant énergétique élastomère thermoplastique d'oxétane, mélangé à une charge explosive à haute énergie de CL-20. Le second agent propulsif comprend un liant énergétique élastomère thermoplastique d'oxétane, mélangé à une charge explosive à haute énergie de RDX. Les plastifiants et les quantités relatives pour les premier et second agents propulsifs sont les mêmes que lorsqu'un seul que pour un seul agent propulsif.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU11597/97A AU1159797A (en) | 1996-11-13 | 1996-11-13 | High energy thermoplastic elastomer propellant |
PCT/US1996/018372 WO1998021168A1 (fr) | 1996-11-13 | 1996-11-13 | Agent propulsif contenant un elastomere thermoplastique a haute energie |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1996/018372 WO1998021168A1 (fr) | 1996-11-13 | 1996-11-13 | Agent propulsif contenant un elastomere thermoplastique a haute energie |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1998021168A1 true WO1998021168A1 (fr) | 1998-05-22 |
Family
ID=22256143
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1996/018372 WO1998021168A1 (fr) | 1996-11-13 | 1996-11-13 | Agent propulsif contenant un elastomere thermoplastique a haute energie |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU1159797A (fr) |
WO (1) | WO1998021168A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003011797A2 (fr) * | 2001-08-01 | 2003-02-13 | Alliant Techsystems Inc. | Compositions explosives de faible sensibilite et procede pour preparer des compositions explosives |
WO2003064351A2 (fr) * | 2001-08-14 | 2003-08-07 | Textron Systems Corporation | Explosif composite plastique a haute performance |
WO2004024653A2 (fr) * | 2002-09-12 | 2004-03-25 | Textron Systems Corporation | Generateur de gaz a plusieurs etages et generateurs de gaz |
US7196099B2 (en) | 2001-09-14 | 2007-03-27 | Aventis Pharmaceuticals Inc. | Compounds and compositions as cathepsin inhibitors |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4091729A (en) * | 1977-03-07 | 1978-05-30 | The United States Of America As Represented By The Secretary Of The Army | Low vulnerability booster charge caseless ammunition |
US4092188A (en) * | 1977-05-16 | 1978-05-30 | Lovelace Alan M Acting Adminis | Nitramine propellants |
US4726919A (en) * | 1985-05-06 | 1988-02-23 | Morton Thiokol, Inc. | Method of preparing a non-feathering nitramine propellant |
US4976794A (en) * | 1988-08-05 | 1990-12-11 | Morton Thiokol Inc. | Thermoplastic elastomer-based low vulnerability ammunition gun propellants |
US5516854A (en) * | 1990-07-27 | 1996-05-14 | Thiokol Corporation | Method of producing thermoplastic elastomers having alternate crystalline structure such as polyoxetane ABA or star block copolymers by a block linking process |
US5529649A (en) * | 1993-02-03 | 1996-06-25 | Thiokol Corporation | Insensitive high performance explosive compositions |
US5565150A (en) * | 1993-12-20 | 1996-10-15 | Thiokol Corporation | Energetic materials processing technique |
-
1996
- 1996-11-13 WO PCT/US1996/018372 patent/WO1998021168A1/fr active Application Filing
- 1996-11-13 AU AU11597/97A patent/AU1159797A/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4091729A (en) * | 1977-03-07 | 1978-05-30 | The United States Of America As Represented By The Secretary Of The Army | Low vulnerability booster charge caseless ammunition |
US4092188A (en) * | 1977-05-16 | 1978-05-30 | Lovelace Alan M Acting Adminis | Nitramine propellants |
US4726919A (en) * | 1985-05-06 | 1988-02-23 | Morton Thiokol, Inc. | Method of preparing a non-feathering nitramine propellant |
US4976794A (en) * | 1988-08-05 | 1990-12-11 | Morton Thiokol Inc. | Thermoplastic elastomer-based low vulnerability ammunition gun propellants |
US5516854A (en) * | 1990-07-27 | 1996-05-14 | Thiokol Corporation | Method of producing thermoplastic elastomers having alternate crystalline structure such as polyoxetane ABA or star block copolymers by a block linking process |
US5529649A (en) * | 1993-02-03 | 1996-06-25 | Thiokol Corporation | Insensitive high performance explosive compositions |
US5565150A (en) * | 1993-12-20 | 1996-10-15 | Thiokol Corporation | Energetic materials processing technique |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003011797A2 (fr) * | 2001-08-01 | 2003-02-13 | Alliant Techsystems Inc. | Compositions explosives de faible sensibilite et procede pour preparer des compositions explosives |
WO2003011797A3 (fr) * | 2001-08-01 | 2003-04-24 | Alliant Techsystems Inc | Compositions explosives de faible sensibilite et procede pour preparer des compositions explosives |
US6881283B2 (en) | 2001-08-01 | 2005-04-19 | Alliant Techsystems Inc. | Low-sensitivity explosive compositions |
WO2003064351A2 (fr) * | 2001-08-14 | 2003-08-07 | Textron Systems Corporation | Explosif composite plastique a haute performance |
WO2003064351A3 (fr) * | 2001-08-14 | 2003-10-30 | Textron Systems Corp | Explosif composite plastique a haute performance |
US7196099B2 (en) | 2001-09-14 | 2007-03-27 | Aventis Pharmaceuticals Inc. | Compounds and compositions as cathepsin inhibitors |
WO2004024653A2 (fr) * | 2002-09-12 | 2004-03-25 | Textron Systems Corporation | Generateur de gaz a plusieurs etages et generateurs de gaz |
WO2004024653A3 (fr) * | 2002-09-12 | 2004-09-23 | Textron Systems Corp | Generateur de gaz a plusieurs etages et generateurs de gaz |
Also Published As
Publication number | Publication date |
---|---|
AU1159797A (en) | 1998-06-03 |
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