DE1250306B - - Google Patents
Info
- Publication number
- DE1250306B DE1250306B DENDAT1250306D DE1250306DA DE1250306B DE 1250306 B DE1250306 B DE 1250306B DE NDAT1250306 D DENDAT1250306 D DE NDAT1250306D DE 1250306D A DE1250306D A DE 1250306DA DE 1250306 B DE1250306 B DE 1250306B
- Authority
- DE
- Germany
- 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.)
- Pending
Links
Classifications
-
- 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
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
-
- 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
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE29735 | 1960-04-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1250306B true DE1250306B (xx) |
Family
ID=3840003
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DENDAT1250306D Pending DE1250306B (xx) | 1960-04-28 |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1250306B (xx) |
| GB (1) | GB977111A (xx) |
| NL (2) | NL124086C (xx) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3998407A (en) * | 1974-07-30 | 1976-12-21 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
| US3986685A (en) * | 1974-07-30 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
| DE3721512C1 (de) * | 1987-06-30 | 1989-03-30 | Diehl Gmbh & Co | Flugkoerper mit ueberkalibrigem Leitwerk |
| DE4020897C2 (de) * | 1990-06-30 | 1993-11-11 | Diehl Gmbh & Co | Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles |
| SE535837C2 (sv) | 2011-04-14 | 2013-01-08 | Bae Systems Bofors Ab | Fenutfällningsmekanism |
-
0
- NL NL264231D patent/NL264231A/xx unknown
- DE DENDAT1250306D patent/DE1250306B/de active Pending
- NL NL124086D patent/NL124086C/xx active
-
1961
- 1961-02-16 GB GB584261A patent/GB977111A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB977111A (en) | 1964-12-02 |
| NL124086C (xx) | |
| NL264231A (xx) |