FR2380529A1 - Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost - Google Patents
Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and costInfo
- Publication number
- FR2380529A1 FR2380529A1 FR7704079A FR7704079A FR2380529A1 FR 2380529 A1 FR2380529 A1 FR 2380529A1 FR 7704079 A FR7704079 A FR 7704079A FR 7704079 A FR7704079 A FR 7704079A FR 2380529 A1 FR2380529 A1 FR 2380529A1
- Authority
- FR
- France
- Prior art keywords
- complexity
- rockets
- missiles
- projectiles
- cost
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- 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
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A propulsive charge for a projectile, missile or rocket is provided with longitudinal elements on its surfaces; the elements are inclined along the longitudinal axis so as to cause the projectile to rotate about that axis. They are made of an inhibiting material, pref. by moulding. Problems associated with divergent vanes are avoided. These problems include increased weight, complexity of mfr, high cost and the need for protection against erosion and temp.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7704079A FR2380529A1 (en) | 1977-02-14 | 1977-02-14 | Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7704079A FR2380529A1 (en) | 1977-02-14 | 1977-02-14 | Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2380529A1 true FR2380529A1 (en) | 1978-09-08 |
FR2380529B1 FR2380529B1 (en) | 1983-09-30 |
Family
ID=9186691
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7704079A Granted FR2380529A1 (en) | 1977-02-14 | 1977-02-14 | Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2380529A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2433730A1 (en) * | 1978-08-16 | 1980-03-14 | Poudres & Explosifs Ste Nale | Pyrotechnic charge which burns at constant pressure - comprises a powder charge disc coated with a combustion inhibitor applied as a pattern of shaped motifs |
RU2451816C1 (en) * | 2010-11-19 | 2012-05-27 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Propellant charge for rocket engine |
RU2464440C1 (en) * | 2011-02-10 | 2012-10-20 | Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" | Solid-fuel charge for rocket engine |
EP2428762A3 (en) * | 2010-09-14 | 2014-12-03 | Diehl BGT Defence GmbH & Co.KG | Propellant charge body |
CN112228247A (en) * | 2020-09-18 | 2021-01-15 | 西北工业大学 | Guide vane type sleeve type grain structure with honeycomb holes |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB141187A (en) * | 1919-04-04 | 1920-04-15 | Garnett Senior | Improvements in and connected with rockets |
CH398414A (en) * | 1959-12-10 | 1966-03-15 | Georg Dr Groetsch | Shaped solid propellant with associated combustion chamber and use of the same |
US3380386A (en) * | 1965-07-16 | 1968-04-30 | Army Usa | Propellant grains |
-
1977
- 1977-02-14 FR FR7704079A patent/FR2380529A1/en active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB141187A (en) * | 1919-04-04 | 1920-04-15 | Garnett Senior | Improvements in and connected with rockets |
CH398414A (en) * | 1959-12-10 | 1966-03-15 | Georg Dr Groetsch | Shaped solid propellant with associated combustion chamber and use of the same |
US3380386A (en) * | 1965-07-16 | 1968-04-30 | Army Usa | Propellant grains |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2433730A1 (en) * | 1978-08-16 | 1980-03-14 | Poudres & Explosifs Ste Nale | Pyrotechnic charge which burns at constant pressure - comprises a powder charge disc coated with a combustion inhibitor applied as a pattern of shaped motifs |
EP2428762A3 (en) * | 2010-09-14 | 2014-12-03 | Diehl BGT Defence GmbH & Co.KG | Propellant charge body |
RU2451816C1 (en) * | 2010-11-19 | 2012-05-27 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Propellant charge for rocket engine |
RU2464440C1 (en) * | 2011-02-10 | 2012-10-20 | Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" | Solid-fuel charge for rocket engine |
CN112228247A (en) * | 2020-09-18 | 2021-01-15 | 西北工业大学 | Guide vane type sleeve type grain structure with honeycomb holes |
Also Published As
Publication number | Publication date |
---|---|
FR2380529B1 (en) | 1983-09-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |