GB1103580A - Fairing - Google Patents
FairingInfo
- Publication number
- GB1103580A GB1103580A GB39614/66A GB3961466A GB1103580A GB 1103580 A GB1103580 A GB 1103580A GB 39614/66 A GB39614/66 A GB 39614/66A GB 3961466 A GB3961466 A GB 3961466A GB 1103580 A GB1103580 A GB 1103580A
- Authority
- GB
- United Kingdom
- Prior art keywords
- staves
- nose cone
- fairing
- missile launcher
- tubular
- 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
- 238000010304 firing Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/06—Rocket or torpedo launchers for rockets from aircraft
- F41F3/065—Rocket pods, i.e. detachable containers for launching a plurality of rockets
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US484820A US3362291A (en) | 1965-09-03 | 1965-09-03 | Fairing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1103580A true GB1103580A (en) | 1968-02-14 |
Family
ID=23925750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB39614/66A Expired GB1103580A (en) | 1965-09-03 | 1966-09-05 | Fairing |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3362291A (enExample) |
| BE (1) | BE686441A (enExample) |
| DE (1) | DE1578017A1 (enExample) |
| GB (1) | GB1103580A (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3670621A (en) * | 1969-10-31 | 1972-06-20 | Alsco Inc | Rocket launcher fairing |
| US3851561A (en) * | 1970-03-25 | 1974-12-03 | Us Navy | Fairing, rocket launcher |
| US4301708A (en) * | 1979-07-25 | 1981-11-24 | The United States Of America As Represented By The Secretary Of The Navy | Launch tube closure |
| US4498368A (en) * | 1983-10-06 | 1985-02-12 | The United States Of America As Representedby The Secretary Of The Navy | Frangible fly through diaphragm for missile launch canister |
| DE3940468A1 (de) * | 1989-12-07 | 1991-06-13 | Telefunken Systemtechnik | Kappe fuer eine raketenaustrittsoeffnung |
| US6311604B1 (en) * | 1990-04-30 | 2001-11-06 | Raytheon Company | Protective missile launch tube enclosure |
| US5162605A (en) * | 1992-01-16 | 1992-11-10 | General Dynamics Corporation | Self-activated rocket launcher cell closure |
| FR2870821B1 (fr) * | 2004-05-25 | 2007-08-17 | Airbus France Sas | Aeronef comprenant un dispositif de detection et/ou de mesure de perturbations atmospheriques |
| US7506572B1 (en) * | 2006-03-27 | 2009-03-24 | The United States Of America As Represented By The Secretary Of The Navy | Combination sabot and launch seal |
| RU2572026C2 (ru) * | 2013-11-07 | 2015-12-27 | Акционерное общество "Авиаагрегат" | Пусковая установка для авиационных ракет |
| US11260957B2 (en) | 2019-02-01 | 2022-03-01 | The Boeing Company | Rupture fairings |
| CN112429280A (zh) * | 2020-12-09 | 2021-03-02 | 北京星际荣耀空间科技股份有限公司 | 一种运载火箭外置摄像头安装结构 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2792754A (en) * | 1952-08-14 | 1957-05-21 | Northrop Aircraft Inc | Rocket tube muzzle door |
| US2826961A (en) * | 1953-04-15 | 1958-03-18 | Acf Ind Inc | Rocket dispensers |
| BE635420A (enExample) * | 1962-07-27 |
-
1965
- 1965-09-03 US US484820A patent/US3362291A/en not_active Expired - Lifetime
-
1966
- 1966-09-05 DE DE19661578017 patent/DE1578017A1/de active Pending
- 1966-09-05 BE BE686441D patent/BE686441A/xx unknown
- 1966-09-05 GB GB39614/66A patent/GB1103580A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE1578017A1 (de) | 1971-02-18 |
| BE686441A (enExample) | 1967-02-15 |
| US3362291A (en) | 1968-01-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1103580A (en) | Fairing | |
| BE608385A (fr) | Empennage à ailettes rétractables pour projectiles à propulsion automatique ou non automatique, et projectile muni de cet empennage. | |
| CA935682A (en) | Salvo-type multiple projectile ammunition and gun for firing the ammunition | |
| GB1024103A (en) | Aircraft with flexible wings | |
| IL29674A (en) | Method of fabricating an explosive projectile head provided with weakening grooves | |
| GB1516073A (en) | Subcalibre projectile | |
| GB697721A (en) | Improvements in or relating to flying bodies | |
| GB793927A (en) | Improvements relating to rocket containers for aircraft | |
| FR2037021A1 (fr) | Lance-bombes sur avion,avec bombes | |
| IL37750A (en) | Exploding missile with dispersible elements,especially missile shot from a barrel | |
| GB1256760A (enExample) | ||
| CA614258A (en) | Jettisonable end cone for aircraft rocket missile pods | |
| JPS52100800A (en) | Electric fuse | |
| GB585782A (en) | Improvements in, or relating to, tails or bridles for rockets | |
| DARWELL et al. | The design of rocket nozzles to reduce gas misalignment(Rocket nozzle design to reduce gas misalignment noting turning moment, nozzle geometry, cold gas tests, static and flight trials of motors, etc) | |
| ES289138U (es) | Cabeza de combate | |
| GB1027919A (en) | Flying body for accommodating military combat means and equipment, and systems formed by these flying bodies | |
| USD208678S (en) | Supersonic airplane | |
| DUGAN | Turbojet and turbofan engines for a mach 3 supersonic transport(Turbojet and turbofan engines for mach 3 supersonic transport aircraft) | |
| GB610685A (en) | Improvements in rockets having sliding tails | |
| CA708904A (en) | Rocket and missile fuel | |
| AU409697B2 (en) | Fuse for a missile to be fired by a gun with rifled bore | |
| CA717288A (en) | Fairing for rocket launchers | |
| GB1227735A (enExample) | ||
| APOSTOLO | Brief review of the aeronautical industry in italy, emphasizing its growth and its dependence on production of military aircraft for exportation |