ATE44314T1 - GROUND LAUNCH FOR MISSILES. - Google Patents
GROUND LAUNCH FOR MISSILES.Info
- Publication number
- ATE44314T1 ATE44314T1 AT87105964T AT87105964T ATE44314T1 AT E44314 T1 ATE44314 T1 AT E44314T1 AT 87105964 T AT87105964 T AT 87105964T AT 87105964 T AT87105964 T AT 87105964T AT E44314 T1 ATE44314 T1 AT E44314T1
- Authority
- AT
- Austria
- Prior art keywords
- missiles
- ground launch
- missile
- movable
- mount
- Prior art date
Links
- 235000015842 Hesperis Nutrition 0.000 abstract 1
- 235000012633 Iberis amara Nutrition 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
- F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Soil Conditioners And Soil-Stabilizing Materials (AREA)
- Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)
- Continuous Casting (AREA)
Abstract
1. Ground launcher for missiles, such as rockets or the like, with a mount carrying the missile, characterized in that on the mount is placed a baffle plate (4) movable in the driving jet (3) of the missile (1) and which under the action of the driving jet (3) is movable into an operative position (15) passing through the entire cross-section thereof.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19863619205 DE3619205A1 (en) | 1986-06-07 | 1986-06-07 | Ground starter for missiles |
| EP87105964A EP0249017B1 (en) | 1986-06-07 | 1987-04-23 | Ground-based launcher for missiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE44314T1 true ATE44314T1 (en) | 1989-07-15 |
Family
ID=6302514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT87105964T ATE44314T1 (en) | 1986-06-07 | 1987-04-23 | GROUND LAUNCH FOR MISSILES. |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0249017B1 (en) |
| AT (1) | ATE44314T1 (en) |
| DE (2) | DE3619205A1 (en) |
| ES (1) | ES2010199B3 (en) |
| GR (1) | GR3000155T3 (en) |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE727060C (en) * | 1935-03-23 | 1942-10-26 | Donar Ges M B H Fuer Appbau | Launch device for missiles |
| US4134327A (en) * | 1977-12-12 | 1979-01-16 | General Dynamics Corporation | Rocket launcher tube post-launch rear closure |
-
1986
- 1986-06-07 DE DE19863619205 patent/DE3619205A1/en not_active Withdrawn
-
1987
- 1987-04-23 AT AT87105964T patent/ATE44314T1/en not_active IP Right Cessation
- 1987-04-23 DE DE8787105964T patent/DE3760286D1/en not_active Expired
- 1987-04-23 ES ES87105964T patent/ES2010199B3/en not_active Expired
- 1987-04-23 EP EP87105964A patent/EP0249017B1/en not_active Expired
-
1989
- 1989-09-15 GR GR89400174T patent/GR3000155T3/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| EP0249017B1 (en) | 1989-06-28 |
| DE3619205A1 (en) | 1987-12-10 |
| ES2010199B3 (en) | 1989-11-01 |
| DE3760286D1 (en) | 1989-08-03 |
| GR3000155T3 (en) | 1990-11-29 |
| EP0249017A1 (en) | 1987-12-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| REN | Ceased due to non-payment of the annual fee |