DE2103844A1 - Abwurfaggregat - Google Patents
AbwurfaggregatInfo
- Publication number
- DE2103844A1 DE2103844A1 DE19712103844 DE2103844A DE2103844A1 DE 2103844 A1 DE2103844 A1 DE 2103844A1 DE 19712103844 DE19712103844 DE 19712103844 DE 2103844 A DE2103844 A DE 2103844A DE 2103844 A1 DE2103844 A1 DE 2103844A1
- Authority
- DE
- Germany
- Prior art keywords
- unit
- control
- fin
- fins
- control fins
- 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.)
- Pending
Links
- 239000003380 propellant Substances 0.000 claims description 17
- 230000000087 stabilizing effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 241000272201 Columbiformes Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
-
- 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
- F42B10/60—Steering arrangements
- F42B10/62—Steering by movement of flight surfaces
- F42B10/64—Steering by movement of flight surfaces of fins
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7005388A FR2079859A5 (enExample) | 1970-02-16 | 1970-02-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2103844A1 true DE2103844A1 (de) | 1971-08-26 |
Family
ID=9050696
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19712103844 Pending DE2103844A1 (de) | 1970-02-16 | 1971-01-27 | Abwurfaggregat |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE2103844A1 (enExample) |
| FR (1) | FR2079859A5 (enExample) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2147725C1 (ru) * | 1999-07-15 | 2000-04-20 | Государственное научно-производственное предприятие "Регион" | Автономный корректируемый летательный аппарат, стабилизированный по крену, с телевизионной головкой самонаведения |
-
1970
- 1970-02-16 FR FR7005388A patent/FR2079859A5/fr not_active Expired
-
1971
- 1971-01-27 DE DE19712103844 patent/DE2103844A1/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| FR2079859A5 (enExample) | 1971-11-12 |
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