FR1418696A - Gouvernail à ailettes pliantes pour fusées - Google Patents
Gouvernail à ailettes pliantes pour fuséesInfo
- Publication number
- FR1418696A FR1418696A FR999953A FR999953A FR1418696A FR 1418696 A FR1418696 A FR 1418696A FR 999953 A FR999953 A FR 999953A FR 999953 A FR999953 A FR 999953A FR 1418696 A FR1418696 A FR 1418696A
- Authority
- FR
- France
- Prior art keywords
- rockets
- folding wing
- wing rudder
- rudder
- folding
- 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
- F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR999953A FR1418696A (fr) | 1963-12-28 | 1964-12-24 | Gouvernail à ailettes pliantes pour fusées |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT2663163 | 1963-12-28 | ||
FR999953A FR1418696A (fr) | 1963-12-28 | 1964-12-24 | Gouvernail à ailettes pliantes pour fusées |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1418696A true FR1418696A (fr) | 1965-11-19 |
Family
ID=26212051
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR999953A Expired FR1418696A (fr) | 1963-12-28 | 1964-12-24 | Gouvernail à ailettes pliantes pour fusées |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1418696A (fr) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2175133A1 (fr) * | 1972-03-08 | 1973-10-19 | Sarmag Sa | |
US3819132A (en) * | 1973-02-21 | 1974-06-25 | Sarmac Sa | Self propelled projectile with fins |
FR2212528A1 (fr) * | 1972-12-30 | 1974-07-26 | Dynamit Nobel Ag | |
US3946969A (en) * | 1974-07-30 | 1976-03-30 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US3952970A (en) * | 1974-08-28 | 1976-04-27 | The United States Of America As Represented By The Secretary Of The Navy | Means for improving rocket missile accuracy |
FR3037390A1 (fr) * | 2015-06-09 | 2016-12-16 | Nexter Munitions | Dispositif de stabilisation et projectile equipe d'un tel dispositif |
CN109141143A (zh) * | 2018-07-26 | 2019-01-04 | 重庆长安工业(集团)有限责任公司 | 一种折叠翼面卡锁机构 |
CN113804066A (zh) * | 2021-09-18 | 2021-12-17 | 天津爱思达航天科技有限公司 | 一种带有同步旋转折叠翼的尾舱结构 |
CN114278465A (zh) * | 2021-12-03 | 2022-04-05 | 西北工业大学太仓长三角研究院 | 一种具有可调式稳定尾翼的微小型火箭推进装置 |
-
1964
- 1964-12-24 FR FR999953A patent/FR1418696A/fr not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2175133A1 (fr) * | 1972-03-08 | 1973-10-19 | Sarmag Sa | |
FR2212528A1 (fr) * | 1972-12-30 | 1974-07-26 | Dynamit Nobel Ag | |
US3819132A (en) * | 1973-02-21 | 1974-06-25 | Sarmac Sa | Self propelled projectile with fins |
US3946969A (en) * | 1974-07-30 | 1976-03-30 | The United States Of America As Represented By The Secretary Of The Army | Folding tail fins |
US3952970A (en) * | 1974-08-28 | 1976-04-27 | The United States Of America As Represented By The Secretary Of The Navy | Means for improving rocket missile accuracy |
FR3037390A1 (fr) * | 2015-06-09 | 2016-12-16 | Nexter Munitions | Dispositif de stabilisation et projectile equipe d'un tel dispositif |
CN109141143A (zh) * | 2018-07-26 | 2019-01-04 | 重庆长安工业(集团)有限责任公司 | 一种折叠翼面卡锁机构 |
CN113804066A (zh) * | 2021-09-18 | 2021-12-17 | 天津爱思达航天科技有限公司 | 一种带有同步旋转折叠翼的尾舱结构 |
CN114278465A (zh) * | 2021-12-03 | 2022-04-05 | 西北工业大学太仓长三角研究院 | 一种具有可调式稳定尾翼的微小型火箭推进装置 |
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