DE977926C - Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature - Google Patents
Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperatureInfo
- Publication number
- DE977926C DE977926C DE1962SC031025 DESC031025A DE977926C DE 977926 C DE977926 C DE 977926C DE 1962SC031025 DE1962SC031025 DE 1962SC031025 DE SC031025 A DESC031025 A DE SC031025A DE 977926 C DE977926 C DE 977926C
- Authority
- DE
- Germany
- Prior art keywords
- oxygen
- binder
- carriers
- organic
- liquid
- 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
Links
Classifications
-
- 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
- C06B21/0083—Treatment of solid structures, e.g. for coating or impregnating with a modifier
Landscapes
- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Organic Chemistry (AREA)
- Air Bags (AREA)
- Solid-Sorbent Or Filter-Aiding Compositions (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Paints Or Removers (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Medicinal Preparation (AREA)
Description
masse des Treibstoffes, erforderlich. Bei der Herstellung von Treibsätzen mit zusätzlichen anorganischen Sauer stoff trägern wird, wie beschrieben, verfahren, nur daß dem Trägersubstanz-flüssige-Sauerstoffträger-Gemisch die anorganischen Sauerstoffträger vor der Zugabe des Chloropren-Polymerisates zugemischt werden.mass of fuel, required. In the production of propellants with additional inorganic Oxygen carriers will proceed as described, except that the carrier substance-liquid-oxygen carrier mixture the inorganic oxygen carriers before the addition of the chloroprene polymer are mixed in.
Bei Verwendung anderer flüssiger Sauerstoffträger als Tetranitromethan, wie z. B. Methylnitrat oder Methylnitrat-Äthylnitrat, erfährt das Verfahren keine Modifikation.When using other liquid oxygen carriers than tetranitromethane, such as. B. methyl nitrate or methyl nitrate-ethyl nitrate, the process is not modified.
Nachfolgend werden noch drei Rezepturbeispiele angeführt:Three recipe examples are given below:
1. 78,3% Tetranitromethan
14% Polyacetylen1. 78.3% tetranitromethane
14% polyacetylene
6,2fl/o Chloropren-Polymerisat6.2 fl / o chloroprene polymer
(ohne Lösungsmittel)
0,3% Butylacetat (Lösungsmittelanteil)
1,2% Methylnitrat (Quellmittel)(without solvent)
0.3% butyl acetate (solvent content)
1.2% methyl nitrate (swelling agent)
2. 46,5% Methylnitrat
32,5% Ammonnitrat
12,2% Aktivkohle2. 46.5% methyl nitrate
32.5% ammonium nitrate
12.2% activated carbon
6,8fl/o Chloropren-Polymerisat6.8 fl / o chloroprene polymer
(ohne Lösungsmittel) o,4°/o Butylacetat (Lösungsmittelanteil) 1,6% Äthylnitrat (Quellmittel) 5(without solvent) 0.4% butyl acetate (solvent content) 1.6% ethyl nitrate (swelling agent) 5
3. 52,4% Methylnitrat
21,2% Äthylnitrat
7,9 °/o Ammonperchlorat
7% Polyacetylen
4% Aktivkohle3. 52.4% methyl nitrate
21.2% ethyl nitrate
7.9 per cent. Ammonium perchlorate
7% polyacetylene
4% activated carbon
5,7°/o Chloropren-Polymerisat5.7% chloroprene polymer
(ohne Lösungsmittel) 0,3 °/o Butylacetat (Lösungsmittelanteil) 0,8% Methylnitrat (Quellmittel) 0,70/0 Äthyl'nitrat (Quellmittel)(without solvent) 0.3% butyl acetate (solvent content) 0.8% methyl nitrate (swelling agent) 0.70 / 0 ethyl nitrate (swelling agent)
Bei Verwendung von festen Chloropren-Polymerisaten sind diese zuerst mit handelsüblichen Lösungsmitteln, denen gegebenenfalls Methylnitrat oder Äthylnitrat zugemischt werden kann, in Lösung zu bringen und die niedrigsiedenden Lösungsmittelanteile, wie oben beschrieben, durch Sprühtrocknung oder Abdampfen zu entfernen.When using solid chloroprene polymers are these first with commercially available solvents, which may be methyl nitrate or ethyl nitrate can be added to bring into solution and the low-boiling solvent components, as described above, to be removed by spray drying or evaporation.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1605107D FR1605107A (en) | 1962-02-20 | 1962-09-07 | Solid propellants - based on liquid comburants absorbed in powdered solids |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DESCH28937A DE977925C (en) | 1960-12-13 | 1960-12-13 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
Publications (1)
Publication Number | Publication Date |
---|---|
DE977926C true DE977926C (en) | 1973-03-22 |
Family
ID=7431269
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DESCH28937A Expired DE977925C (en) | 1960-12-13 | 1960-12-13 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
DE1960977931D Expired DE977931C (en) | 1960-12-13 | 1960-12-14 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
DE1962SC031025 Expired DE977926C (en) | 1960-12-13 | 1962-02-20 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DESCH28937A Expired DE977925C (en) | 1960-12-13 | 1960-12-13 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
DE1960977931D Expired DE977931C (en) | 1960-12-13 | 1960-12-14 | Process for the production of composite propellants using liquid oxygen carriers that are stable at normal temperature |
Country Status (1)
Country | Link |
---|---|
DE (3) | DE977925C (en) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB864749A (en) * | 1955-07-26 | 1961-04-06 | Gen Tire & Rubber Co | Solid rocket fuel and method of manufacture |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE352839C (en) * | 1922-05-05 | A Wohl Dr | Manufacture of explosives | |
DE352838C (en) * | 1919-01-15 | 1922-05-05 | A Wohl Dr | Manufacture of explosives |
DE391821C (en) * | 1921-11-12 | 1924-03-11 | Hans P Kaufmann Dr | Process for the production of new explosives mixtures |
DE410525C (en) * | 1923-09-06 | 1925-03-09 | Elek Zitaetswerk Lonza Fa | Process for the manufacture of explosives |
DE419127C (en) * | 1924-08-08 | 1925-09-21 | Alfred Wohl Dr | Explosive mix |
US2920949A (en) * | 1943-12-30 | 1960-01-12 | Morris S Kharasch | Process of producing an incendiary composition |
US3012866A (en) * | 1945-12-22 | 1961-12-12 | Aerojet General Co | Propellant for rocket motors |
-
1960
- 1960-12-13 DE DESCH28937A patent/DE977925C/en not_active Expired
- 1960-12-14 DE DE1960977931D patent/DE977931C/en not_active Expired
-
1962
- 1962-02-20 DE DE1962SC031025 patent/DE977926C/en not_active Expired
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB864749A (en) * | 1955-07-26 | 1961-04-06 | Gen Tire & Rubber Co | Solid rocket fuel and method of manufacture |
Also Published As
Publication number | Publication date |
---|---|
DE977931C (en) | 1973-03-22 |
DE977925C (en) | 1973-03-22 |
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