ES345609A1 - Rocket motor using a double-base propellant - Google Patents
Rocket motor using a double-base propellantInfo
- Publication number
- ES345609A1 ES345609A1 ES345609A ES345609A ES345609A1 ES 345609 A1 ES345609 A1 ES 345609A1 ES 345609 A ES345609 A ES 345609A ES 345609 A ES345609 A ES 345609A ES 345609 A1 ES345609 A1 ES 345609A1
- Authority
- ES
- Spain
- Prior art keywords
- lead
- acid
- base propellant
- resorcylate
- double
- 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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/007—Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
-
- 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
- F02K9/18—Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Air Bags (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
- Medicinal Preparation (AREA)
- Inorganic Compounds Of Heavy Metals (AREA)
- Testing Of Engines (AREA)
Abstract
A double base propellant comprises nitrocellulose and nitroglycerine, or dimethylene glycol dinitrate, or methyltrimethylol methane trinitrate, or diethylene glycol dinitrate, or metriol trinitrate, and additives selected from salicylic acid, # - resorcylic acid, 2,5 - dihydroxy - benzoic acid, 5 - methylene disalicylic acid, powdered aluminium, lead salicylate, lead acetylsalicylate, lead 2,4 - dihydroxybenzoate, lead 2 - ethylhexoate, propyl - di - N - adipate, 2 - nitrodiphenylamine, monobasic cupric salicylate, monobasic lead # - resorcylate, candelilla wax, cupric # - resorcylate and aliphatic or aromatic salts of lead and/or copper.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE2046551 | 1967-02-22 | ||
BE2046724 | 1967-04-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES345609A1 true ES345609A1 (en) | 1970-02-01 |
Family
ID=25661642
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES345609A Expired ES345609A1 (en) | 1967-02-22 | 1967-09-30 | Rocket motor using a double-base propellant |
Country Status (12)
Country | Link |
---|---|
AT (1) | AT277669B (en) |
AU (1) | AU5549973A (en) |
BE (2) | BE694408A (en) |
CH (1) | CH489706A (en) |
DE (1) | DE1626083A1 (en) |
DK (1) | DK141607C (en) |
ES (1) | ES345609A1 (en) |
GB (1) | GB1204138A (en) |
GR (1) | GR33273B (en) |
LU (1) | LU54389A1 (en) |
NL (1) | NL6712608A (en) |
NO (1) | NO122959B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2193491B (en) * | 1978-07-21 | 1988-09-14 | Imi Kynoch Limited Kynoch Work | Improvements in propellants |
-
1967
- 1967-02-22 BE BE694408D patent/BE694408A/xx not_active IP Right Cessation
- 1967-04-10 BE BE696817D patent/BE696817A/xx unknown
- 1967-08-28 LU LU54389A patent/LU54389A1/xx unknown
- 1967-08-30 DE DE1967F0053352 patent/DE1626083A1/en active Pending
- 1967-09-04 AT AT08097/67A patent/AT277669B/en not_active IP Right Cessation
- 1967-09-04 NO NO169597A patent/NO122959B/no unknown
- 1967-09-12 GR GR670133273A patent/GR33273B/en unknown
- 1967-09-13 CH CH1284967A patent/CH489706A/en not_active IP Right Cessation
- 1967-09-14 NL NL6712608A patent/NL6712608A/xx unknown
- 1967-09-30 ES ES345609A patent/ES345609A1/en not_active Expired
- 1967-10-04 GB GB4530267A patent/GB1204138A/en not_active Expired
- 1967-10-12 DK DK506867A patent/DK141607C/en not_active IP Right Cessation
-
1973
- 1973-05-10 AU AU55499/73A patent/AU5549973A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
NL6712608A (en) | 1968-08-23 |
AT277669B (en) | 1970-01-12 |
DE1626083A1 (en) | 1970-04-02 |
GB1204138A (en) | 1970-09-03 |
CH489706A (en) | 1970-04-30 |
DK141607C (en) | 1980-10-13 |
DK141607B (en) | 1980-05-05 |
NO122959B (en) | 1971-09-06 |
BE694408A (en) | 1967-08-22 |
GR33273B (en) | 1967-11-18 |
AU5549973A (en) | 1974-11-14 |
BE696817A (en) | 1967-10-10 |
LU54389A1 (en) | 1967-10-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES345609A1 (en) | Rocket motor using a double-base propellant | |
IT945912B (en) | THRUST INVERTERS FOR GAS TURBINE ENGINES | |
IT1019001B (en) | IMPROVEMENT IN SOLID PROPELLENT CHARGES FOR ROCKET ENGINES | |
GB1247713A (en) | Phenylglycine derivatives | |
PH10111A (en) | Explosive compositions comprising aluminum sensitizers | |
SE8501809L (en) | Fuel | |
GB1114878A (en) | Improvements in or relating to rocket propellant charges | |
CA734501A (en) | Recovery of nitroglycerine from spent nitrating acids | |
MY7300321A (en) | Rocket motor using a double-base propellant | |
US3872158A (en) | Oxalacetic acid bis(2-substituted-2,2-dinitroethyl)esters | |
IT976741B (en) | EXPLOSIVE PROPELLENT CONTAINING TRIAMMINOGUANIDINE NITRATE | |
ES202752A1 (en) | Improvements in rocket motors | |
IT1235560B (en) | NITROCELLULOSE FREE POWDER FOR PROPELLANT CHARGE | |
NL173958C (en) | PROCESS FOR PREPARING A HYDROHALOGENIDE FROM AN ESTER OF 7-AMINO-3METHYL-3-CEFEM-4-CARBONIC ACID. | |
GB1007926A (en) | Improvements in or relating to complex lead salts and explosive compositions | |
FR1492452A (en) | Process for preparing a solid propellant composition | |
GB1081732A (en) | New cellulose derivatives | |
BRUNK | Energetic discussion of the theory of frictional collision according to Routh | |
BE773788A (en) | HIGH POWER EXPLOSIVE SLURRIES BASED ON NITROGLYCEROGLYCOL | |
ENGEL et al. | Synthesis of lead salicylates(double base rocket propellants moderators) | |
Eaton | Regarding Practical Points | |
SE7503833L (en) | TRANSPORT LINE FOR EXPLOSIVE GAS. | |
ES194507Y (en) | RIGID SAFETY CONTAINER FOR FINE EXPLOSIVE POWDERS, ESPECIALLY THOSE OF NITROCELLULOSE. | |
CA715815A (en) | Blasting explosive cartridges containing ethylene glycol dinitrate | |
AU2355162A (en) | Blasting explosive cartridges containing ethylene glycol dinitrate |