FR1307270A - Tailplane for projectile and method of assembly - Google Patents
Tailplane for projectile and method of assemblyInfo
- Publication number
- FR1307270A FR1307270A FR864302A FR864302A FR1307270A FR 1307270 A FR1307270 A FR 1307270A FR 864302 A FR864302 A FR 864302A FR 864302 A FR864302 A FR 864302A FR 1307270 A FR1307270 A FR 1307270A
- Authority
- FR
- France
- Prior art keywords
- tailplane
- projectile
- assembly
- 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
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/04—Rifle grenades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR864302A FR1307270A (en) | 1961-06-08 | 1961-06-08 | Tailplane for projectile and method of assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR864302A FR1307270A (en) | 1961-06-08 | 1961-06-08 | Tailplane for projectile and method of assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1307270A true FR1307270A (en) | 1962-10-26 |
Family
ID=8756809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR864302A Expired FR1307270A (en) | 1961-06-08 | 1961-06-08 | Tailplane for projectile and method of assembly |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1307270A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3532300A (en) * | 1967-03-17 | 1970-10-06 | Dynamit Nobel Ag | Fin-stabilized projectile having an improved annular fin assembly |
FR2436962A1 (en) * | 1978-09-22 | 1980-04-18 | Sarmac Sa | EXPLOSIVE RIFLE GRENADE |
EP0049738A2 (en) * | 1980-10-09 | 1982-04-21 | Rheinmetall GmbH | Armour-piercing projectile having stabilizing fins |
FR2561764A1 (en) * | 1984-03-21 | 1985-09-27 | Losfeld Christian | Economic projectile for mortar |
FR2599829A1 (en) * | 1986-06-05 | 1987-12-11 | France Etat Armement | EMPTYING FOR PROJECTILE WITH KINETIC ENERGY OF THE FLECHE TYPE |
WO1988007169A1 (en) * | 1987-03-17 | 1988-09-22 | The Secretary Of State For Defence In Her Britanni | Tail fin unit for a projectile |
US4978088A (en) * | 1988-12-19 | 1990-12-18 | Diehl Gmbh & Co. | Guidance mechanism for a subcaliber-sized fin-stabilized practice projectile |
US5158509A (en) * | 1990-12-14 | 1992-10-27 | The United States Of America As Represented By The United States Department Of Energy | Composite stabilizer unit |
EP1731871A1 (en) * | 2005-06-07 | 2006-12-13 | Diehl BGT Defence GmbH & Co.KG | Wing assembly and missile |
-
1961
- 1961-06-08 FR FR864302A patent/FR1307270A/en not_active Expired
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3532300A (en) * | 1967-03-17 | 1970-10-06 | Dynamit Nobel Ag | Fin-stabilized projectile having an improved annular fin assembly |
FR2436962A1 (en) * | 1978-09-22 | 1980-04-18 | Sarmac Sa | EXPLOSIVE RIFLE GRENADE |
EP0049738A2 (en) * | 1980-10-09 | 1982-04-21 | Rheinmetall GmbH | Armour-piercing projectile having stabilizing fins |
EP0049738A3 (en) * | 1980-10-09 | 1982-04-28 | Rheinmetall Gmbh | Armour-piercing projectile having stabilizing fins |
FR2561764A1 (en) * | 1984-03-21 | 1985-09-27 | Losfeld Christian | Economic projectile for mortar |
EP0249525A1 (en) * | 1986-06-05 | 1987-12-16 | ETAT-FRANCAIS représenté par le DELEGUE GENERAL POUR L'ARMEMENT (DPAG) | Stabilization fins for an arrow-type penetrator |
FR2599829A1 (en) * | 1986-06-05 | 1987-12-11 | France Etat Armement | EMPTYING FOR PROJECTILE WITH KINETIC ENERGY OF THE FLECHE TYPE |
WO1988007169A1 (en) * | 1987-03-17 | 1988-09-22 | The Secretary Of State For Defence In Her Britanni | Tail fin unit for a projectile |
GB2228987A (en) * | 1987-03-17 | 1990-09-12 | Secr Defence | Tail fin unit for a projectile |
GB2228987B (en) * | 1987-03-17 | 1991-01-23 | Secr Defence | Tail fin unit for a projectile |
US4978088A (en) * | 1988-12-19 | 1990-12-18 | Diehl Gmbh & Co. | Guidance mechanism for a subcaliber-sized fin-stabilized practice projectile |
US5158509A (en) * | 1990-12-14 | 1992-10-27 | The United States Of America As Represented By The United States Department Of Energy | Composite stabilizer unit |
EP1731871A1 (en) * | 2005-06-07 | 2006-12-13 | Diehl BGT Defence GmbH & Co.KG | Wing assembly and missile |
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