DE1771943C2 - Ignition kit for propellants and rocket propellants - Google Patents
Ignition kit for propellants and rocket propellantsInfo
- Publication number
- DE1771943C2 DE1771943C2 DE1771943A DE1771943A DE1771943C2 DE 1771943 C2 DE1771943 C2 DE 1771943C2 DE 1771943 A DE1771943 A DE 1771943A DE 1771943 A DE1771943 A DE 1771943A DE 1771943 C2 DE1771943 C2 DE 1771943C2
- Authority
- DE
- Germany
- Prior art keywords
- ignition
- powder
- propellant
- charges
- firing
- 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
- 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
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C7/00—Non-electric detonators; Blasting caps; Primers
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C9/00—Chemical contact igniters; Chemical lighters
Description
In vielen Fällen ist somit ein der jeweiligen Muni- sätzen.In many cases, this is one of the respective ammunition.
lionstemperatur entsprechendes Einrichten der Waffe 55 Die erfindungsgemäßen Anfeuerungssätze könnenlion temperature appropriate setup of the weapon 55 The ignition sets according to the invention can
erforderlich, was nicht nur bei Kartusch-Munition sowohl in mehr oder weniger gepreßter als auch gra-required, which is not only required for cartridge ammunition in both more or less compressed and
und Raketen, sondern auch bei rückstoßfreien Waffen nulierter Form hergestellt und eingesetzt werden, jeand missiles, but also with recoilless weapons of nulated form are manufactured and used, depending
hinderlich ist, bei denen beispielsweise nach Art der nachdem, wie es für den betreffenden Anwendungsfallis a hindrance in which, for example, according to the type of after how it is for the application in question
bekannten Panzerfaust-Typen panzerbrechende Hohl- vorteilhaft ist.known Panzerfaust types armor piercing hollow is advantageous.
ladungsgeschosse, mit oder ohne Nachbeschleunigun- 60 Eventuell auftretende höhere Gasdrücke könnenprojectiles, with or without post-acceleration
gen derselben durch einen Raketentreibsatz, aus einem durch Reduzieren des Gesamtgewichtes des Anfeue-the same by a rocket propellant, from one by reducing the total weight of the
beiderseits offenen Lancier-Rohr verschossen werden, rungssatzes ohne Nachteile für seine prä/.ise Funktioncan be fired on both sides with an open lancet tube, without any disadvantages for its pre / .ise function
wobei der Vortrieb der Geschosse durch eine im Ge- abgebaut werden.the propulsion of the storeys being dismantled by an in the building.
schoßende untergebrachte Treibmittelladung bewirkt Als Binderanteil kann in der Heißpartikelzündwird, deren Druckwelle sich gegen die Druckwelle 65 masse auch Nitrocellulose, Leim, Stärke oder Gummieiner gleichzeitig gezündeten, im h'nteren Teil des arabikum enthalten sein. Art Stelle von elementarem Lander-Rohres untergebrachten Tieibmittelladung Bor kann der erfinilungsgemäße Anfeuerungssatz mit Verdammung abstützt. auch Legierungen oder intermetallische Phasen desfiring propellant charge caused as a binder component in the hot particle ignition, whose pressure wave also masses against the pressure wave 65, nitrocellulose, glue, starch or rubber liner at the same time ignited, to be contained in the lower part of the arabic. Kind of place of elementary Lander-Rohres housed tie-medium charge boron can be the firing set according to the invention propped up with damnation. also alloys or intermetallic phases of the
Bors mit Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Co, Ni wnd anderen Übergangselementen enthalten, Gegebenenfalls können in dem Anfeuerungssatz noch Flußmittel, wie z. B. Calciumfluorid, Magnesiumoxyd sowie Gleitmittel, wie z. B. Stearat oder Wachse, vorhanden sein.Bors with Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Co, Ni wnd contain other transition elements, if applicable can still flux such. B. calcium fluoride, magnesium oxide and Lubricants such as B. stearate or waxes may be present.
Die Zusammensetzung eines für Anfeuerungen geeigneten Schwarzpulvers sowie einer geeigneten Heißpartikelzöndmasse sind in dem folgenden Anwendungsbeispiel angegeben:The composition of a black powder suitable for firing and a suitable hot particle igniter are given in the following application example:
a) Schwarzpulver für Anfeuerungssätzea) Black powder for cheering kits
Zusamemnsetzung:Composition:
etwa 75 Gewichtsprozent Kaliumnitrat,
etwa 10 Gewichtsprozent Schwefel, etwa 15 Gewichtsprozent Holzkohle.about 75 percent by weight potassium nitrate,
about 10 weight percent sulfur, about 15 weight percent charcoal.
b) Heißpartikelzündmasse des Anfeuerungssatzesb) Hot particle ignition mass of the ignition kit
Zusammensetzung:
etwa 24 Gewichtsprozent Bor, amorph,Composition:
about 24 percent by weight boron, amorphous,
etwa 70 Gewichtsprozent Kaliumnitrat,
wasserfrei,about 70 percent by weight potassium nitrate,
anhydrous,
etwa 6 Gewichtsprozent Binder, bestehend aus 90,13 Gewichtsprozent eines zähflüssigen, vorpolymerisierten Diisocyanate aus Toluylendiisocyanat und 1,4-Butandiol mit einem mittleren Molekulargewicht von etwa 2000 und einem mittleren Isocyanatgehalt von etwa 4% (Adiprene L100) und 9,87 Gewichtsprozent Methylen-bjs-o-chloranilin. about 6 percent by weight binder, consisting of 90.13 percent by weight of a viscous, prepolymerized diisocyanates from toluene diisocyanate and 1,4-butanediol with an average molecular weight of about 2000 and an average isocyanate content of about 4% (Adiprene L100) and 9.87% by weight methylene-bjs-o-chloroaniline.
Claims (3)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1771943A DE1771943C2 (en) | 1968-08-05 | 1968-08-05 | Ignition kit for propellants and rocket propellants |
NL6911485A NL6911485A (en) | 1968-08-05 | 1969-07-25 | |
FR6926757A FR2015074A1 (en) | 1968-08-05 | 1969-08-04 | |
BE737055D BE737055A (en) | 1968-08-05 | 1969-08-04 | |
GB39244/69A GB1279680A (en) | 1968-08-05 | 1969-08-05 | Improvements in or relating to primer compositions |
US847701A US3682727A (en) | 1968-08-05 | 1969-08-05 | Igniter charge for propellant compositions and rocket propellant charges |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1771943A DE1771943C2 (en) | 1968-08-05 | 1968-08-05 | Ignition kit for propellants and rocket propellants |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1771943B1 DE1771943B1 (en) | 1972-05-31 |
DE1771943C2 true DE1771943C2 (en) | 1975-03-27 |
Family
ID=5701045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1771943A Expired DE1771943C2 (en) | 1968-08-05 | 1968-08-05 | Ignition kit for propellants and rocket propellants |
Country Status (6)
Country | Link |
---|---|
US (1) | US3682727A (en) |
BE (1) | BE737055A (en) |
DE (1) | DE1771943C2 (en) |
FR (1) | FR2015074A1 (en) |
GB (1) | GB1279680A (en) |
NL (1) | NL6911485A (en) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3862865A (en) * | 1971-05-24 | 1975-01-28 | Kilgore Corp | Sparkler composition |
US3905846A (en) * | 1973-05-23 | 1975-09-16 | Us Navy | Composite modified double base propellant with metal oxide stabilizer |
US3986910A (en) * | 1974-04-12 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Navy | Composite propellants containing critical pressure increasing additives |
US4167428A (en) * | 1974-05-17 | 1979-09-11 | The United States Of America As Represented By The Secretary Of The Army | Conductance method for determining the mechanical properties of propellants |
US4021514A (en) * | 1974-06-21 | 1977-05-03 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Method for the production of an inhibitor coating for a solid rocket propellent charge |
CH602519A5 (en) * | 1974-06-21 | 1978-07-31 | Oerlikon Buehrle Ag | |
DE2820969C1 (en) * | 1978-05-12 | 1991-12-05 | Bayern Chemie Gmbh Flugchemie | Solid composite fuel with stable combustion |
US4412874A (en) * | 1981-11-19 | 1983-11-01 | The United States Of America As Represented By The Secretary Of The Army | Silane ballistic modifier containing propellant |
US4332631A (en) * | 1982-03-04 | 1982-06-01 | Hercules Incorporated | Castable silicone based magnesium fueled propellant |
DE3243425A1 (en) * | 1982-11-24 | 1984-05-24 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V., 8000 München | Igniter for propellant charges |
DE3245907C2 (en) * | 1982-12-11 | 1986-10-30 | Diehl GmbH & Co, 8500 Nürnberg | Process for the production of an incendiary mixture and its use in ammunition |
FR2650586B1 (en) * | 1989-08-01 | 1991-10-11 | France Etat Armement | IGNITION COMPOSITION FOR PYROTECHNIC DELAY |
US5368662A (en) * | 1992-09-29 | 1994-11-29 | Thiokol Corporation | TPE binder containing crystalline modifiers and solid propellants based thereon |
JP3543347B2 (en) * | 1994-01-24 | 2004-07-14 | 日本油脂株式会社 | Method for producing igniter granules |
US20010030007A1 (en) | 1994-09-13 | 2001-10-18 | Gunther Faber | Ignition elements and finely graduatable ignition components |
DE59509947D1 (en) * | 1994-09-13 | 2002-01-24 | Dynamit Nobel Ag | IGNITION ELEMENTS AND FINE-STAGGABLE IGNITIONS |
DE19548544A1 (en) * | 1995-12-23 | 1997-06-26 | Dynamit Nobel Ag | Ignition mixture free of initial explosives |
DE19616627A1 (en) * | 1996-04-26 | 1997-11-06 | Dynamit Nobel Ag | Kindling mixtures |
DE59608681D1 (en) * | 1996-12-13 | 2002-03-14 | Ruag Munition Thun | Pyrotechnic delay element, process for its production and its use |
US6224099B1 (en) * | 1997-07-22 | 2001-05-01 | Cordant Technologies Inc. | Supplemental-restraint-system gas generating device with water-soluble polymeric binder |
US6170399B1 (en) | 1997-08-30 | 2001-01-09 | Cordant Technologies Inc. | Flares having igniters formed from extrudable igniter compositions |
BR9812622A (en) * | 1997-09-04 | 2000-08-22 | Cordant Tech Inc | Lighting devices having ignition agents formed from ignition compositions that can be extruded |
US6045726A (en) * | 1998-07-02 | 2000-04-04 | Atlantic Research Corporation | Fire suppressant |
US6086693A (en) * | 1999-02-02 | 2000-07-11 | Autoliv Asp, Inc. | Low particulate igniter composition for a gas generant |
DE50015593D1 (en) * | 1999-12-03 | 2009-04-23 | Ruag Ammotec Gmbh | IGNITION DEVICE FOR DRIFTING POWDER |
GB2450750B (en) * | 2007-07-06 | 2012-08-29 | Paul Smith | Surface-modified magnesium powders for use in pyrotechnic compositions |
EP2240422B1 (en) * | 2007-12-24 | 2016-12-21 | General Dynamics Ordnance and Tactical Systems - Canada Inc. | Low toxicity primer composition for reduced energy ammunition |
RU2501776C1 (en) * | 2012-07-19 | 2013-12-20 | Открытое акционерное общество "Чебоксарское производственное объединение им. В.И. Чапаева" | Pyrotechnic igniter composition |
US20180370868A1 (en) * | 2015-11-09 | 2018-12-27 | The Johns Hopkins University | Composite reactive materials with independently controllable ignition and combustion properties |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942547A (en) * | 1958-06-24 | 1960-06-28 | Olin Mathieson | Gas generating assembly |
DE1187167B (en) * | 1963-02-23 | 1965-02-11 | Nitrochemie Ges Mit Beschraenk | Extrudable, smokeless or low-smoke burning propellant |
-
1968
- 1968-08-05 DE DE1771943A patent/DE1771943C2/en not_active Expired
-
1969
- 1969-07-25 NL NL6911485A patent/NL6911485A/xx unknown
- 1969-08-04 BE BE737055D patent/BE737055A/xx unknown
- 1969-08-04 FR FR6926757A patent/FR2015074A1/fr not_active Withdrawn
- 1969-08-05 GB GB39244/69A patent/GB1279680A/en not_active Expired
- 1969-08-05 US US847701A patent/US3682727A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE1771943B1 (en) | 1972-05-31 |
GB1279680A (en) | 1972-06-28 |
US3682727A (en) | 1972-08-08 |
FR2015074A1 (en) | 1970-04-24 |
NL6911485A (en) | 1970-02-09 |
BE737055A (en) | 1970-01-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE1771943C2 (en) | Ignition kit for propellants and rocket propellants | |
DE1918046A1 (en) | Igniter | |
DE3043805A1 (en) | WEAPON OR ARRANGEMENT FOR FIREING PROJECTILE | |
DE2008156C1 (en) | Protective device against projectiles | |
DE2733700C2 (en) | Training warhead for artillery missiles | |
EP2151422A2 (en) | Weapon for selective causation of a detonation or deflagration | |
DE2552950A1 (en) | Incendiary ammunition | |
DE2414310C2 (en) | ||
DE3243425C2 (en) | ||
DE2458877C2 (en) | Combustible protective cover against thermal influences for projectile propellants for automatic weapons | |
DE2329665A1 (en) | NON-FATAL FLOOR | |
DE3245907C2 (en) | Process for the production of an incendiary mixture and its use in ammunition | |
DE2830119A1 (en) | FUEL CHARGE FOR ROCKETS AND SHELLS | |
DE3242106C1 (en) | Propellent charge compositions for barrel-type weapons | |
DE3630019C2 (en) | ||
DE300650C (en) | ||
DE4204318A1 (en) | DRIVE CHARGE MODULE | |
DE2752844A1 (en) | Missile warhead usable at various ranges - has propellant charge in sections which can be fired in part or fully | |
WO1999035108A1 (en) | Propellant explosive | |
DE3048941A1 (en) | Mortar bomb guidance mechanism - has vanes held folded by combustible sleeve | |
DE1446924C1 (en) | Pourable solid rocket propellant containing ammonium nitrate | |
DE1099804B (en) | Two-stage rocket with a combustible base stage | |
DE2604757A1 (en) | Ballistic fusion warhead projectile - has launcher forming integral fuse device for thermonuclear warhead | |
DE1553996A1 (en) | Arrangement for recoilless guns | |
DE2555104A1 (en) | Caseless ammunition for automatic firearms - has compacted propellant charge with embedded bullet held in magazine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
E77 | Valid patent as to the heymanns-index 1977 |