BE520064A - - Google Patents
Info
- Publication number
- BE520064A BE520064A BE520064DA BE520064A BE 520064 A BE520064 A BE 520064A BE 520064D A BE520064D A BE 520064DA BE 520064 A BE520064 A BE 520064A
- Authority
- BE
- Belgium
- Prior art keywords
- projectile
- fins
- projectile according
- nozzle
- deflector
- Prior art date
Links
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 239000007789 gas Substances 0.000 description 16
- 239000003381 stabilizer Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 230000006641 stabilisation Effects 0.000 description 3
- 238000011105 stabilization Methods 0.000 description 3
- 206010013710 Drug interaction Diseases 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000000126 substance Substances 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
- F42B10/02—Stabilising arrangements
- F42B10/26—Stabilising arrangements using spin
- F42B10/28—Stabilising arrangements using spin induced by gas action
- F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE520064A true BE520064A (no) |
Family
ID=156080
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE520064D BE520064A (no) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE520064A (no) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4673146A (en) * | 1983-08-15 | 1987-06-16 | General Dynamics, Pomona Division | Missile tail fin assembly |
| US5806791A (en) * | 1995-05-26 | 1998-09-15 | Raytheon Company | Missile jet vane control system and method |
| US6676072B1 (en) * | 2002-11-13 | 2004-01-13 | Steven S. Kim | Short duration, high-torque rocket nozzle |
-
0
- BE BE520064D patent/BE520064A/fr unknown
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4673146A (en) * | 1983-08-15 | 1987-06-16 | General Dynamics, Pomona Division | Missile tail fin assembly |
| US5806791A (en) * | 1995-05-26 | 1998-09-15 | Raytheon Company | Missile jet vane control system and method |
| US6676072B1 (en) * | 2002-11-13 | 2004-01-13 | Steven S. Kim | Short duration, high-torque rocket nozzle |
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