GB994184A - Improvements in or relating to propellent grains - Google Patents
Improvements in or relating to propellent grainsInfo
- Publication number
- GB994184A GB994184A GB2572561A GB2572561A GB994184A GB 994184 A GB994184 A GB 994184A GB 2572561 A GB2572561 A GB 2572561A GB 2572561 A GB2572561 A GB 2572561A GB 994184 A GB994184 A GB 994184A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sodium
- potassium
- ammonium
- barium
- propellent
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/26—Burning control
-
- 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
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/10—Shape or structure of solid propellant charges
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Crystallography & Structural Chemistry (AREA)
- Organic Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
In a propellent grain having embedded therein one or more elongated heat-conducting units (see Division F3), the propellent may be plastic and comprise (a) polyvinyl chloride, dibutyl sebacate, and ammonium nitrate or perchlorate; copper chromite may be added as a burning catalyst; (b) nitrocellulose, nitroglycerine, diethyl phthalate, 2-nitrodiphenylamine, and candelilla wax; (c) finely-divided ammonium, sodium, or potassium perchlorate or nitrate, or barium peroxide, dispersed in a liquid fuel, e.g. triethyl benzene, dodecane, liquid polyisobutylene, dimethyl maleate, diethyl phthalate, dibutyl oxalate, benzyl alcohol, triethylene glycol, and methyl-naphthyl ether; also present may be aluminium or magnesium powder and a gelling agent, e.g. polyvinyl chloride, polyvinyl acetate, ethyl cellulose, cellulose acetate, or sodium or magnesium stearate or palmitate. A self-oxidant composition, used for coating the metal units to vary the burning rate, may comprise nitrocellulose gelatinized with nitroglycerine or with a plasticizer, many of which are specified; other coating compositions comprise an oxidant, and a binding agent, to which may be added organic fuels, finely-divided metals, carbon, or silicon. Suitable oxidants are ammonium, potassium, sodium and lithium chlorates and perchlorates, ammonium, potassium, sodium and barium nitrates, peroxides of lead, barium, potassium, and sodium, hexanitroethane, mannitol hexanitrate, and RDX, and suitable binding agents are organic polymers, natural and synthetic rubbers, natural resins, silicones and bituminous materials.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2572561A GB994184A (en) | 1961-07-15 | 1961-07-15 | Improvements in or relating to propellent grains |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2572561A GB994184A (en) | 1961-07-15 | 1961-07-15 | Improvements in or relating to propellent grains |
Publications (1)
Publication Number | Publication Date |
---|---|
GB994184A true GB994184A (en) | 1965-06-02 |
Family
ID=10232277
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2572561A Expired GB994184A (en) | 1961-07-15 | 1961-07-15 | Improvements in or relating to propellent grains |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB994184A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193491A (en) * | 1978-07-21 | 1988-02-10 | Imi Kynoch Limited Kynoch Work | Propellants |
EP0724551A1 (en) * | 1993-10-22 | 1996-08-07 | Thiokol Corporation | Use of carbon fibrils to enhance burn rate of pyrotechnics and gas generants |
US10415938B2 (en) | 2017-01-16 | 2019-09-17 | Spectre Enterprises, Inc. | Propellant |
CN112196692A (en) * | 2020-10-14 | 2021-01-08 | 中国人民解放军国防科技大学 | A fuel-rich electronically controlled solid ramjet with continuously adjustable electrode combustible thrust |
CN112855385A (en) * | 2021-01-08 | 2021-05-28 | 西安近代化学研究所 | Charging structure suitable for low-temperature ignition |
US11112222B2 (en) | 2019-01-21 | 2021-09-07 | Spectre Materials Sciences, Inc. | Propellant with pattern-controlled burn rate |
US11530669B2 (en) * | 2020-09-11 | 2022-12-20 | Raytheon Company | Variable burn-rate solid rocket motor ignition method |
US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
WO2023192061A1 (en) * | 2022-03-31 | 2023-10-05 | Raytheon Company | Propulsion system with grooved inert rods for reactive wire |
US12234198B2 (en) | 2021-08-04 | 2025-02-25 | Spectre Enterprises, Inc. | Passivated fuel |
-
1961
- 1961-07-15 GB GB2572561A patent/GB994184A/en not_active Expired
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193491A (en) * | 1978-07-21 | 1988-02-10 | Imi Kynoch Limited Kynoch Work | Propellants |
EP0724551A1 (en) * | 1993-10-22 | 1996-08-07 | Thiokol Corporation | Use of carbon fibrils to enhance burn rate of pyrotechnics and gas generants |
EP0724551A4 (en) * | 1993-10-22 | 1997-04-23 | Thiokol Corp | Use of carbon fibrils to enhance burn rate of pyrotechnics and gas generants |
US10415938B2 (en) | 2017-01-16 | 2019-09-17 | Spectre Enterprises, Inc. | Propellant |
US11112222B2 (en) | 2019-01-21 | 2021-09-07 | Spectre Materials Sciences, Inc. | Propellant with pattern-controlled burn rate |
US11530669B2 (en) * | 2020-09-11 | 2022-12-20 | Raytheon Company | Variable burn-rate solid rocket motor ignition method |
CN112196692A (en) * | 2020-10-14 | 2021-01-08 | 中国人民解放军国防科技大学 | A fuel-rich electronically controlled solid ramjet with continuously adjustable electrode combustible thrust |
CN112855385A (en) * | 2021-01-08 | 2021-05-28 | 西安近代化学研究所 | Charging structure suitable for low-temperature ignition |
CN112855385B (en) * | 2021-01-08 | 2022-03-29 | 西安近代化学研究所 | Charging structure suitable for low-temperature ignition |
US11650037B2 (en) | 2021-02-16 | 2023-05-16 | Spectre Materials Sciences, Inc. | Primer for firearms and other munitions |
US12234198B2 (en) | 2021-08-04 | 2025-02-25 | Spectre Enterprises, Inc. | Passivated fuel |
WO2023192061A1 (en) * | 2022-03-31 | 2023-10-05 | Raytheon Company | Propulsion system with grooved inert rods for reactive wire |
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