FR2146649A6 - Solid-fuel rocket primer - comprising silicone elastomer body for use at very low temps - Google Patents
Solid-fuel rocket primer - comprising silicone elastomer body for use at very low tempsInfo
- Publication number
- FR2146649A6 FR2146649A6 FR7126792A FR7126792A FR2146649A6 FR 2146649 A6 FR2146649 A6 FR 2146649A6 FR 7126792 A FR7126792 A FR 7126792A FR 7126792 A FR7126792 A FR 7126792A FR 2146649 A6 FR2146649 A6 FR 2146649A6
- Authority
- FR
- France
- Prior art keywords
- primer
- dia
- solid
- silicone elastomer
- cavities
- 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
- 229920002379 silicone rubber Polymers 0.000 title abstract 2
- 239000004449 solid propellant Substances 0.000 title abstract 2
- 239000008188 pellet Substances 0.000 abstract 2
- 235000015842 Hesperis Nutrition 0.000 abstract 1
- 235000012633 Iberis amara Nutrition 0.000 abstract 1
- MUBZPKHOEPUJKR-UHFFFAOYSA-N Oxalic acid Chemical compound OC(=O)C(O)=O MUBZPKHOEPUJKR-UHFFFAOYSA-N 0.000 abstract 1
- 230000007257 malfunction Effects 0.000 abstract 1
- 239000004033 plastic Substances 0.000 abstract 1
- 229920003023 plastic Polymers 0.000 abstract 1
- 229920001296 polysiloxane Polymers 0.000 abstract 1
- 239000000843 powder Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0823—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
- F42C19/0826—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators
-
- 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
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0819—Primers or igniters for the initiation of rocket motors, i.e. pyrotechnical aspects thereof
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
A primer for solid-fuel rockets, which does not malfunction at temps. as low as -40 degrees C, comprises a flexible silicone elastomer cylinder having an axial bore for the primary charge, >=1 ring of cylindrical cavities disposed regularly round the bore with radial perforations connecting these cavities to the exterior of the flexible cylinder. The primary charge is cannon-type black powder contained in a perforated sheath having a plastics envelope, detonated by a electric igniter via a pyrotechnic system, or by a wholly pyrotechnic system. The primary charge consists of aluminothermic pellets disposed uniformly in the cavities. Specif. the cavity dia. is about the same as that of the pellets, which is 0.1-30 mm, and the cavity dia. is pref. 0.1-0.4 times the primer dia. The silicone may be filled with Ca oxalate.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7126792A FR2146649A6 (en) | 1968-04-10 | 1971-07-22 | Solid-fuel rocket primer - comprising silicone elastomer body for use at very low temps |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR147595 | 1968-04-10 | ||
FR7126792A FR2146649A6 (en) | 1968-04-10 | 1971-07-22 | Solid-fuel rocket primer - comprising silicone elastomer body for use at very low temps |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2146649A6 true FR2146649A6 (en) | 1973-03-02 |
Family
ID=26181938
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7126792A Expired FR2146649A6 (en) | 1968-04-10 | 1971-07-22 | Solid-fuel rocket primer - comprising silicone elastomer body for use at very low temps |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2146649A6 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2325900A1 (en) * | 1975-09-27 | 1977-04-22 | Rheinmetall Gmbh | PRIMING CHAIN |
EP0580017A1 (en) * | 1992-07-18 | 1994-01-26 | DIEHL GMBH & CO. | Igniter for propulsive charges |
-
1971
- 1971-07-22 FR FR7126792A patent/FR2146649A6/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2325900A1 (en) * | 1975-09-27 | 1977-04-22 | Rheinmetall Gmbh | PRIMING CHAIN |
EP0580017A1 (en) * | 1992-07-18 | 1994-01-26 | DIEHL GMBH & CO. | Igniter for propulsive charges |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property |