US2780997A - Smokeless powder grains and method of making same - Google Patents
Smokeless powder grains and method of making same Download PDFInfo
- Publication number
- US2780997A US2780997A US358216A US35821653A US2780997A US 2780997 A US2780997 A US 2780997A US 358216 A US358216 A US 358216A US 35821653 A US35821653 A US 35821653A US 2780997 A US2780997 A US 2780997A
- Authority
- US
- United States
- Prior art keywords
- crystallites
- smokeless powder
- orientation
- cellulose
- molecules
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
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
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
- C06B21/0033—Shaping the mixture
- C06B21/0066—Shaping the mixture by granulation, e.g. flaking
Definitions
- the present invention relates to the manufacture of smokeless powder grains and more particularly to the manufacture of such grains. having greater mechanical strength than has heretofore been attained, making them more suitable for use as a rocket fuel.
- This application is a division of application Serial No. 138,073, now matured into Patent No. 2,668,132, filed January 11, 1950, for Smokeless Powder Grains and Method of Making Same.
- p t c A fuel commonly employed for the propulsion of rockets is smokeless powder, one of whose chief constituents is cellulose nitrate.
- the usual method of preparing the fuel charges for rocket propulsion consists of forming a plurality of grains of desired size and shape from a plastic mass of cellulose nitrate in a suitable solvent, said mass including the various other constituents of the charge, such as a nitrate salt and/ or nitroglycerine or the like, dissolved therein or in suspension.
- a nitrate salt and/ or nitroglycerine or the like dissolved therein or in suspension.
- Another object of the present invention is to provide a smokeless powder grain of superior mechanical strength than has heretofore been known.
- Another object of the present invention is to provide a smokeless powder grain comprising" a plurality of laminae having oriented cellulose nitrate crystallitesor molecules in each lamina, and alternatively having laminae with non-oriented crystallites interdispersed among the laminae having oriented crystallites.
- a further object of the present invention is to provide a smokeless powder wafer having uniaxial and/or uniplanar orientation of its cellulose nitrate crystallites.
- a still further object of the present invention is to provide a smokeless powder grain comprising a mat of smokeless powder filaments, each filament having oriented cellulose nitrate crystallites, and alternatively being interwoven with other filaments whose crystallites are not so oriented.
- a still further object of the present invention is to provide a process for producing uniaxial and/or uniplanar orientation of the molecules or crystallites of cellulose esters such as cellulose nitrate, acetate, butyrate, acetate butyrate, acetate propionate and the like and other cellulose compounds.
- a still further object of the present invention is to provide a grain comprising a plurality of sections of a cellu- Patented Feb. 12, 1957 2 lose compound, each section having uniaxial and/or uniplanar orientation of its cellulosic crystallites or molecules, and alternatively having sections with non-oriented cellulosic crystallites'or molecules interdispersed among the sections having oriented crystallites .or molecules.
- Smokeless powder is usuallyformed of cellulose nitrate or a like cellulosic ester having suspended or otherwise contained therein various other constituents, such as nitrate salts and/or nitroglycerine or the like.
- grains of such a smokeless powder are made by forming a plastic composition of the cellulose nitrate by dissolving it in a suitable solvent such as acetone, alcohol, ether, or the like and introducing into said plastic composition the other desired constituents of smokeless powder. This composition is then extruded from a die or the like, the extrusion being, carried out at high shear.
- the extrusion may be in the form of a sheet, ribbon, or filament or any other desired shape provided a high shear is maintained atthe extrusion nozzle.
- the extruded form is then dried, while being maintained under tension along the line of extrusion during the drying step. This process. results in substantially uniaxial orientation of the cellulose nitrate crystallites or molecules.
- the above process is equally applicable to other cellulose compounds such as acetate, butyrate, acetate propionate, acetate butyrate and the like.
- the extrusion of the plastic mass in the above described process should be carried out, at rates of shear greater than second and at shearing stresses greater than 100 p. s. i. through orifices of /5; inch or less when the viscosity of the material being extruded is greater than 10 poises.
- the temperature in the drying step should be such that the extrusion rapidly attains a value of greater than 10 poises.
- the tension maintained on the extrusion during the drying step is critical only for the brief time in which the viscosity is low and during this time should be relatively great, preferably near the breaking strength of the hot ribbon.
- the sufiiciency of the shear during the extrusion process to produce the desired orientation can be determined by X-ray examination of the product, due to the X-ray scattering eifect caused by the orientation of the crystallites or molecules.
- cellulose nitrate and other cellulose compounds having their crystallites or molecules oriented along an axis, present greater mechanical strength along the axis of orientation than can be obtained from commensurate samples of cellulose esters having random orientatlon of their crystallites or molecules. Since it is desirable, as discussed above, to have grains of smokeless powder of high mechanical strength for the fuel charge for rockets, the present invention contemplates in addition to the foregoing process, the advantages to be derived therefrom in producing smokeless powder grains from the product of the above process.
- a ribbon of smokeless powder, or other mixture containing a cellulose ester or other cellulose compound amenable to the above process is formed according to the foregoing process to produce uniaxially oriented crystallites or molecules therein.
- the dried ribbon is then divided into particles, sections or waters of uniform size.
- Several of these wafers are then laminated together such that the axis of crystallite or molecular orientation of each lamina is preferably in a different direction from the axis of each other lamina.
- the resultant grain then has greater mechanical Strength along the lines of these various axes than can be obtained by a random orientation of the crystallites or molecules.
- the lamination step may be carried out by any conventional process such as by merely applying pressure to the stacked particles or by coating the surfaces of each particle with a small quantity of solvent, stacking the pieces, and then drying the product.
- Unoriented laminae may, if desired, be interdispersed among the oriented laminae, sufficient mechanical strength being supplied by the latter to insure a sufiiciently strong grain.
- a filament of smokeless powder,'or other mixture containing a cellulose ester or other cellulose compound amenable to the above process, whose crystallites'or molecules have been oriented acccrdingto the process described above is produced, and then the filament is divided into a plurality of shorter fibers or sections which are then formed into a mat by any conventional process, the various fibers or sections being placed in the mat to provide for axes of orientation in a plurality of directions.
- the grain formed thereby is afforded greater mechanical strength than can be obtained from random orientation of the crystallites or molecules as in the previously described embodiment.
- fibers whose crystallites or molecules are randomly oriented may be intermingled with the uniaxially oriented fibers.
- This embodiment may also be applied to ribbons having oriented crystallites or molecules, as well as fibers,'to produce a mat as here described.
- a still further embodiment of the present invention involves an additional step to the above described process for producing uniaxially oriented crystallites, namely that a ribbon, sheet, or filament of cellulose nitrate, or other cellulose compound such as acetate, butyrate, and the like, having uniaxially oriented crystallites may be'given a uniplanar orientation of said crystallites in addition to uniaxial orientation by rolling or pressing the uniaxially oriented product to from one-third to one-fifth its original thickness or less.
- This process is limited to cellulose compounds which possess crystallites in their structures and is not generally applicable to molecular orientation as in the preceding process.
- a charge of smokeless powder may be formed having great mechanical strength along the axis and in the plane of orientation of the crystallites thereof.
- the ribbon or sheet or the like of smokeless powder, or other cellulose compound amenable to the latter process, having its crystallites thus oriented may be divided into particles, sections, wafers, or fibers or the like, and if desired various wafers may be laminated together or various fibers or ribbons may be matted together as above described, thereby forming a smokeless powder grain having the axis of orientationof various wafers or fibers on different lines from those of other wafers or fibers, and thereby imparting to the wafer great mechanical strength along each of the said axes and along the plane of orientation.
- the uniplanar orientation above discussed may be accomplished independently of the uniaxial orientation, and when so done is not dependent upon the existence of crystallites as in the combined uniplanar and uniaxial orientation.
- the uniplanar orientation process may, therefore, be. applied to cellulose nitrate and other cellulose compounds such as acetate, butyrate, acetate butyrate, acetate propionate, and the like to produce grains thereof, as above described, having great mechanical strength due t to the uniplanar orientation of the molecules or crystallites thereof.
- a smokeless powder grain may be formed suitable for use as a motive fuel charge for rockets, and having such mechanical strength as substantially to eliminate the fragmentation or fracture of the grain due to the shock waves that traverse the charge on ignition, thereby imparting reproducible and predictable ballistic characteristics to the rocket flight.
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Processes Of Treating Macromolecular Substances (AREA)
Description
United States Patent 2,780,997 SMOKELESS rowonn GRAINS AND OF MAKING SAME METHOD No Drawing. Original application January 11,1950, Se-
rial No. 138,073, now Patent No. 2,668,132, dated February 2, 1954. Divided and this application May' 22, 1953, Serial No. 358,216
1 Claim. ci. 102-9 The present invention relates to the manufacture of smokeless powder grains and more particularly to the manufacture of such grains. having greater mechanical strength than has heretofore been attained, making them more suitable for use as a rocket fuel. This application is a division of application Serial No. 138,073, now matured into Patent No. 2,668,132, filed January 11, 1950, for Smokeless Powder Grains and Method of Making Same. p t c A fuel commonly employed for the propulsion of rockets is smokeless powder, one of whose chief constituents is cellulose nitrate. The usual method of preparing the fuel charges for rocket propulsion consists of forming a plurality of grains of desired size and shape from a plastic mass of cellulose nitrate in a suitable solvent, said mass including the various other constituents of the charge, such as a nitrate salt and/ or nitroglycerine or the like, dissolved therein or in suspension. In order to determine the ballistic characteristics of a rocket, it is necessary that each charge be controlled and uniform. Heretofore such determinations have been ,unreliable chiefly because of the fragmentation and fracturing of the grains during the burning of the fuel charge resulting in non-uniform combustion thereof.
It is therefore oneobject of this invention to provide smokeless powder grains that are superior to those heretofore produced, in that they oifer greater resistance to fracture and fragmentation during ignition thereof, yielding determinable and reproducible ballistic characteristics of a rocket when employed as a propellant therefor.
Another object of the present invention is to provide a smokeless powder grain of superior mechanical strength than has heretofore been known.
Another object of the present invention is to provide a smokeless powder grain comprising" a plurality of laminae having oriented cellulose nitrate crystallitesor molecules in each lamina, and alternatively having laminae with non-oriented crystallites interdispersed among the laminae having oriented crystallites.
A further object of the present invention is to provide a smokeless powder wafer having uniaxial and/or uniplanar orientation of its cellulose nitrate crystallites.
A still further object of the present invention is to provide a smokeless powder grain comprising a mat of smokeless powder filaments, each filament having oriented cellulose nitrate crystallites, and alternatively being interwoven with other filaments whose crystallites are not so oriented.
A still further object of the present invention is to provide a process for producing uniaxial and/or uniplanar orientation of the molecules or crystallites of cellulose esters such as cellulose nitrate, acetate, butyrate, acetate butyrate, acetate propionate and the like and other cellulose compounds.
A still further object of the present invention is to provide a grain comprising a plurality of sections of a cellu- Patented Feb. 12, 1957 2 lose compound, each section having uniaxial and/or uniplanar orientation of its cellulosic crystallites or molecules, and alternatively having sections with non-oriented cellulosic crystallites'or molecules interdispersed among the sections having oriented crystallites .or molecules.
Smokeless powder is usuallyformed of cellulose nitrate or a like cellulosic ester having suspended or otherwise contained therein various other constituents, such as nitrate salts and/or nitroglycerine or the like. According to the present invention grains of such a smokeless powder are made by forming a plastic composition of the cellulose nitrate by dissolving it in a suitable solvent such as acetone, alcohol, ether, or the like and introducing into said plastic composition the other desired constituents of smokeless powder. This composition is then extruded from a die or the like, the extrusion being, carried out at high shear. The extrusion may be in the form of a sheet, ribbon, or filament or any other desired shape provided a high shear is maintained atthe extrusion nozzle. The extruded form is then dried, while being maintained under tension along the line of extrusion during the drying step. This process. results in substantially uniaxial orientation of the cellulose nitrate crystallites or molecules. The above process is equally applicable to other cellulose compounds such as acetate, butyrate, acetate propionate, acetate butyrate and the like.
in the above process, when substances whose structure includes crystallites are used, .both crystallite and molecular orientation is obtained, but in the case of cellulose compounds not possessing crystallites, such as the mixed esters and highly plasticized cellulose esters such as compounded cellulose nitrate, the same desired properties are obtained by the molecular orientation in the absence of crystallites. p
To obtain suitable orientation of the crystallites or molecules of the cellulose compound, the extrusion of the plastic mass in the above described process should be carried out, at rates of shear greater than second and at shearing stresses greater than 100 p. s. i. through orifices of /5; inch or less when the viscosity of the material being extruded is greater than 10 poises. The temperature in the drying step should be such that the extrusion rapidly attains a value of greater than 10 poises. The tension maintained on the extrusion during the drying step is critical only for the brief time in which the viscosity is low and during this time should be relatively great, preferably near the breaking strength of the hot ribbon. The sufiiciency of the shear during the extrusion process to produce the desired orientation can be determined by X-ray examination of the product, due to the X-ray scattering eifect caused by the orientation of the crystallites or molecules.
It has been found that cellulose nitrate and other cellulose compounds, having their crystallites or molecules oriented along an axis, present greater mechanical strength along the axis of orientation than can be obtained from commensurate samples of cellulose esters having random orientatlon of their crystallites or molecules. Since it is desirable, as discussed above, to have grains of smokeless powder of high mechanical strength for the fuel charge for rockets, the present invention contemplates in addition to the foregoing process, the advantages to be derived therefrom in producing smokeless powder grains from the product of the above process.
In one embodiment of this invention derived from the above described process, a ribbon of smokeless powder, or other mixture containing a cellulose ester or other cellulose compound amenable to the above process, is formed according to the foregoing process to produce uniaxially oriented crystallites or molecules therein. The dried ribbon is then divided into particles, sections or waters of uniform size. Several of these wafers are then laminated together such that the axis of crystallite or molecular orientation of each lamina is preferably in a different direction from the axis of each other lamina. The resultant grain then has greater mechanical Strength along the lines of these various axes than can be obtained by a random orientation of the crystallites or molecules.
The lamination step may be carried out by any conventional process such as by merely applying pressure to the stacked particles or by coating the surfaces of each particle with a small quantity of solvent, stacking the pieces, and then drying the product. Unoriented laminae may, if desired, be interdispersed among the oriented laminae, sufficient mechanical strength being supplied by the latter to insure a sufiiciently strong grain.
In another embodiment of the present invention a filament of smokeless powder,'or other mixture containing a cellulose ester or other cellulose compound amenable to the above process, whose crystallites'or molecules have been oriented acccrdingto the process described above is produced, and then the filament is divided into a plurality of shorter fibers or sections which are then formed into a mat by any conventional process, the various fibers or sections being placed in the mat to provide for axes of orientation in a plurality of directions. The grain formed thereby is afforded greater mechanical strength than can be obtained from random orientation of the crystallites or molecules as in the previously described embodiment. Also, if desired, fibers whose crystallites or molecules are randomly oriented may be intermingled with the uniaxially oriented fibers. This embodiment may also be applied to ribbons having oriented crystallites or molecules, as well as fibers,'to produce a mat as here described.
A still further embodiment of the present invention involves an additional step to the above described process for producing uniaxially oriented crystallites, namely that a ribbon, sheet, or filament of cellulose nitrate, or other cellulose compound such as acetate, butyrate, and the like, having uniaxially oriented crystallites may be'given a uniplanar orientation of said crystallites in addition to uniaxial orientation by rolling or pressing the uniaxially oriented product to from one-third to one-fifth its original thickness or less. This process, however, is limited to cellulose compounds which possess crystallites in their structures and is not generally applicable to molecular orientation as in the preceding process. Thus a charge of smokeless powder may be formed having great mechanical strength along the axis and in the plane of orientation of the crystallites thereof.
As in the case of the above described embodiments, the ribbon or sheet or the like of smokeless powder, or other cellulose compound amenable to the latter process, having its crystallites thus oriented may be divided into particles, sections, wafers, or fibers or the like, and if desired various wafers may be laminated together or various fibers or ribbons may be matted together as above described, thereby forming a smokeless powder grain having the axis of orientationof various wafers or fibers on different lines from those of other wafers or fibers, and thereby imparting to the wafer great mechanical strength along each of the said axes and along the plane of orientation.
The uniplanar orientation above discussed may be accomplished independently of the uniaxial orientation, and when so done is not dependent upon the existence of crystallites as in the combined uniplanar and uniaxial orientation. The uniplanar orientation process may, therefore, be. applied to cellulose nitrate and other cellulose compounds such as acetate, butyrate, acetate butyrate, acetate propionate, and the like to produce grains thereof, as above described, having great mechanical strength due t to the uniplanar orientation of the molecules or crystallites thereof.
It is thus apparent that by use of any of the foregoing embodiments of the present invention a smokeless powder grain may be formed suitable for use as a motive fuel charge for rockets, and having such mechanical strength as substantially to eliminate the fragmentation or fracture of the grain due to the shock waves that traverse the charge on ignition, thereby imparting reproducible and predictable ballistic characteristics to the rocket flight.
The embodiments of the present invention herein described are only illustrative thereof. Other embodiments and modifications of the present invention within the spirit and scope of the appended claim will be apparent to those skilled in the art.
What is claimed is:
The process of producing a smokeless powder grain of great physical strength consisting of extruding a cellulose nitrate composition under high shear suflicient to produce detectable orientation of the molecules from wafers, and laminating said smokeless powder wafers to form said grain with diversified axes of uniaxial molecular orientation such that said grain has the characteristics of uniform combustion without fracture and fragmentation.
References Cited in the file of this patent UNITED STATES PATENTS 1,784,758 Sheppard et al. Dec. 9, 1930 1,808,998 Sheppard et al. June 9, 1931 2,000,013 Dreyfus et al. May 7, 1935 2,655,694 Piper Oct. 20, 1953
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US358216A US2780997A (en) | 1950-01-11 | 1953-05-22 | Smokeless powder grains and method of making same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US138073A US2668132A (en) | 1950-01-11 | 1950-01-11 | Smokeless powder grains and method of making same |
US358216A US2780997A (en) | 1950-01-11 | 1953-05-22 | Smokeless powder grains and method of making same |
Publications (1)
Publication Number | Publication Date |
---|---|
US2780997A true US2780997A (en) | 1957-02-12 |
Family
ID=26835843
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US358216A Expired - Lifetime US2780997A (en) | 1950-01-11 | 1953-05-22 | Smokeless powder grains and method of making same |
Country Status (1)
Country | Link |
---|---|
US (1) | US2780997A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2933041A (en) * | 1954-04-12 | 1960-04-19 | Phillips Petroleum Co | Rocket grain |
US3032975A (en) * | 1957-03-25 | 1962-05-08 | Phillips Petroleum Co | Rocket motor |
US3745927A (en) * | 1969-05-19 | 1973-07-17 | Celanese Corp | Casing and propellant of nitrocellulose filaments and nitrocellulose fibers |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1784758A (en) * | 1929-02-02 | 1930-12-09 | Eastman Kodak Co | Cellulose film |
US1808998A (en) * | 1930-01-30 | 1931-06-09 | Eastman Kodak Co | Cellulose film |
US2000013A (en) * | 1931-11-05 | 1935-05-07 | Celanese Corp | Method of producing artificial straw and product thereof |
US2655694A (en) * | 1945-07-28 | 1953-10-20 | William E Piper | Manufacture of smokeless powder |
-
1953
- 1953-05-22 US US358216A patent/US2780997A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1784758A (en) * | 1929-02-02 | 1930-12-09 | Eastman Kodak Co | Cellulose film |
US1808998A (en) * | 1930-01-30 | 1931-06-09 | Eastman Kodak Co | Cellulose film |
US2000013A (en) * | 1931-11-05 | 1935-05-07 | Celanese Corp | Method of producing artificial straw and product thereof |
US2655694A (en) * | 1945-07-28 | 1953-10-20 | William E Piper | Manufacture of smokeless powder |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2933041A (en) * | 1954-04-12 | 1960-04-19 | Phillips Petroleum Co | Rocket grain |
US3032975A (en) * | 1957-03-25 | 1962-05-08 | Phillips Petroleum Co | Rocket motor |
US3745927A (en) * | 1969-05-19 | 1973-07-17 | Celanese Corp | Casing and propellant of nitrocellulose filaments and nitrocellulose fibers |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2417090A (en) | Manufacture of propellent explosives | |
US4072546A (en) | Use of graphite fibers to augment propellant burning rate | |
US3897733A (en) | High bulk density extruded propellant for small arms cartridges | |
US3745927A (en) | Casing and propellant of nitrocellulose filaments and nitrocellulose fibers | |
DE2245510A1 (en) | FLOATING MASS FOR HELLLESS EXPLOSIVE DRIVING CHARGES AND PROCESS FOR THEIR PRODUCTION | |
US3348445A (en) | Method of making solid propellants in textile form | |
US2780997A (en) | Smokeless powder grains and method of making same | |
GB1605251A (en) | Propellent powder bodies and process for the production thereof | |
US3014796A (en) | Solid composite propellants containing chlorinated polyphenols and method of preparation | |
DE2412523A1 (en) | PYROTECHNICAL SUBSTANCES AND THE PROCESS FOR THEIR PRODUCTION | |
US2668132A (en) | Smokeless powder grains and method of making same | |
DE1279316B (en) | Use of mechanically comminuted cellulose crystallite aggregates for the production of shock and heat-resistant molded bodies | |
RU2382019C1 (en) | Block propellant porous charge (versions) and method of its manufacturing | |
US3282146A (en) | Method of making combustible cartridge cases | |
US2742672A (en) | Process for preparing composite propellants | |
US2466597A (en) | Nonmetallic armor | |
US3269880A (en) | Heat resistant butadiene-acrylonitrile propellants | |
DE1809360A1 (en) | INSULATING COMPOUNDS FOR THE PRODUCTION OF AN INSULATING LAYER ON SOLIDS MISSILE DEPLOYMENT AND ITS USE FOR THE PRODUCTION OF THIS INSULATION LAYER | |
US3856590A (en) | Propellants and method of producing the same | |
US3304867A (en) | Solid propellants in textile form | |
US3405201A (en) | Process for preparing propellant grain | |
US2495216A (en) | Method of manufacturing propellants | |
US5831339A (en) | Continuous process for solvent-free manufacture of heat-curable composite pyrotechnic products | |
DE10027413B4 (en) | A method of making a blowing agent composition using a dry blending method | |
US2333637A (en) | Explosive composition |