FR1505851A - Ailettes de stabilisation et de guidage repliables pour fusées - Google Patents
Ailettes de stabilisation et de guidage repliables pour fuséesInfo
- Publication number
- FR1505851A FR1505851A FR88021A FR88021A FR1505851A FR 1505851 A FR1505851 A FR 1505851A FR 88021 A FR88021 A FR 88021A FR 88021 A FR88021 A FR 88021A FR 1505851 A FR1505851 A FR 1505851A
- Authority
- FR
- France
- Prior art keywords
- rockets
- guide fins
- stabilization
- folding
- folding stabilization
- 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
- 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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5396665 | 1965-12-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1505851A true FR1505851A (fr) | 1967-12-15 |
Family
ID=10469555
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR88021A Expired FR1505851A (fr) | 1965-12-20 | 1966-12-19 | Ailettes de stabilisation et de guidage repliables pour fusées |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1505851A (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0013096A1 (fr) * | 1978-12-29 | 1980-07-09 | The Commonwealth Of Australia | Mécanisme pour aile repliable |
FR2448707A1 (fr) * | 1979-02-08 | 1980-09-05 | British Aerospace | Ensemble a ailettes repliables pour engin volant |
DE3441534A1 (de) * | 1984-11-14 | 1986-05-15 | Diehl GmbH & Co, 8500 Nürnberg | Lageranordnung fuer das ruderblatt eines flugkoerpers |
WO1988005898A1 (fr) * | 1987-02-02 | 1988-08-11 | Eskam, Armin | Projectile ou missile empenne |
EP0506536A1 (fr) * | 1991-03-26 | 1992-09-30 | Societe D'applications Generales D'electricite Et De Mecanique Sagem | Dispositif de déplacement d'une ailette d'un projectile |
WO1995031689A1 (fr) * | 1994-05-13 | 1995-11-23 | Hughes Aircraft Company | Missile a ailettes de guidage deployables |
WO2006081226A1 (fr) * | 2005-01-26 | 2006-08-03 | Raytheon Company | Systeme de deploiement d'ailettes monoaxial |
-
1966
- 1966-12-19 FR FR88021A patent/FR1505851A/fr not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0013096A1 (fr) * | 1978-12-29 | 1980-07-09 | The Commonwealth Of Australia | Mécanisme pour aile repliable |
FR2448707A1 (fr) * | 1979-02-08 | 1980-09-05 | British Aerospace | Ensemble a ailettes repliables pour engin volant |
DE3441534A1 (de) * | 1984-11-14 | 1986-05-15 | Diehl GmbH & Co, 8500 Nürnberg | Lageranordnung fuer das ruderblatt eines flugkoerpers |
WO1988005898A1 (fr) * | 1987-02-02 | 1988-08-11 | Eskam, Armin | Projectile ou missile empenne |
EP0506536A1 (fr) * | 1991-03-26 | 1992-09-30 | Societe D'applications Generales D'electricite Et De Mecanique Sagem | Dispositif de déplacement d'une ailette d'un projectile |
FR2674619A1 (fr) * | 1991-03-26 | 1992-10-02 | Sagem | Dispositif de deplacement d'une ailette d'un projectile. |
WO1995031689A1 (fr) * | 1994-05-13 | 1995-11-23 | Hughes Aircraft Company | Missile a ailettes de guidage deployables |
WO2006081226A1 (fr) * | 2005-01-26 | 2006-08-03 | Raytheon Company | Systeme de deploiement d'ailettes monoaxial |
US7642492B2 (en) | 2005-01-26 | 2010-01-05 | Raytheon Company | Single-axis fin deployment system |
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