DE3004509A1 - Faltflossenaufbau fuer einen flugkoerper - Google Patents
Faltflossenaufbau fuer einen flugkoerperInfo
- Publication number
- DE3004509A1 DE3004509A1 DE19803004509 DE3004509A DE3004509A1 DE 3004509 A1 DE3004509 A1 DE 3004509A1 DE 19803004509 DE19803004509 DE 19803004509 DE 3004509 A DE3004509 A DE 3004509A DE 3004509 A1 DE3004509 A1 DE 3004509A1
- Authority
- DE
- Germany
- Prior art keywords
- axis
- fin
- turntable
- base plate
- missile
- 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.)
- Withdrawn
Links
- 238000010276 construction Methods 0.000 title description 2
- 210000002435 tendon Anatomy 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 4
- 210000001520 comb Anatomy 0.000 claims 1
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization 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
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7904561 | 1979-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3004509A1 true DE3004509A1 (de) | 1980-08-21 |
Family
ID=10503067
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19803004509 Withdrawn DE3004509A1 (de) | 1979-02-08 | 1980-02-07 | Faltflossenaufbau fuer einen flugkoerper |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3004509A1 (OSRAM) |
FR (1) | FR2448707A1 (OSRAM) |
GB (1) | GB2041502B (OSRAM) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2150092B (en) * | 1983-11-25 | 1987-07-22 | British Aerospace | Deployment and actuation mechanisms |
GB2155157B (en) * | 1984-02-17 | 1987-08-12 | Hunting Eng Ltd | Helix ring devices and assemblies including them |
IL107844A (en) * | 1993-12-02 | 1996-06-18 | Ministry Of Defence Armaments | Flying object control system |
US5829715A (en) * | 1996-04-19 | 1998-11-03 | Lockheed Martin Vought Systems Corp. | Multi-axis unfolding mechanism with rate controlled synchronized movement |
US6092264A (en) * | 1998-11-13 | 2000-07-25 | Lockheed Martin Corporation | Single axis fold actuator and lock for member |
FR2797946B1 (fr) * | 1999-08-31 | 2002-10-04 | Aerospatiale Matra Missiles | Dispositif de montage d'un appendice rigide sur un engin apte a etre lance depuis le tube, et engin correspondant |
FR2916268B1 (fr) * | 2007-05-15 | 2010-09-10 | Saint Louis Inst | Projectile et procede de pilotage associe |
CN113108652B (zh) * | 2021-04-13 | 2022-09-27 | 哈尔滨工程大学 | 一种导弹舵面旋转折叠收放结构 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3063375A (en) * | 1960-05-19 | 1962-11-13 | Wilbur W Hawley | Folding fin |
FR1505851A (fr) * | 1965-12-20 | 1967-12-15 | United Kingdom Government | Ailettes de stabilisation et de guidage repliables pour fusées |
GB1187035A (en) * | 1966-08-02 | 1970-04-08 | British Aircraft Corp Ltd | Aerial Guided Missiles with Fins. |
CH479849A (it) * | 1967-07-22 | 1969-10-15 | Bombrini Parodi Delfino Spa | Porietto autopropulso o semiautopropulso con governale ad alette retrattili |
-
1980
- 1980-01-24 GB GB8002192A patent/GB2041502B/en not_active Expired
- 1980-02-07 FR FR8002710A patent/FR2448707A1/fr active Granted
- 1980-02-07 DE DE19803004509 patent/DE3004509A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
FR2448707A1 (fr) | 1980-09-05 |
FR2448707B1 (OSRAM) | 1983-11-25 |
GB2041502B (en) | 1982-09-08 |
GB2041502A (en) | 1980-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8127 | New person/name/address of the applicant |
Owner name: BRITISH AEROSPACE PLC, LONDON, GB |
|
8140 | Disposal/non-payment of the annual fee for main application |