ATE78335T1 - SELF-PROPELLED PROJECTILE AND A LAUNCHING DEVICE EQUIPPED WITH A PYROTECHNIC IGNITION SYSTEM, INCLUDING SUCH A PROJECTILE. - Google Patents
SELF-PROPELLED PROJECTILE AND A LAUNCHING DEVICE EQUIPPED WITH A PYROTECHNIC IGNITION SYSTEM, INCLUDING SUCH A PROJECTILE.Info
- Publication number
- ATE78335T1 ATE78335T1 AT88400829T AT88400829T ATE78335T1 AT E78335 T1 ATE78335 T1 AT E78335T1 AT 88400829 T AT88400829 T AT 88400829T AT 88400829 T AT88400829 T AT 88400829T AT E78335 T1 ATE78335 T1 AT E78335T1
- Authority
- AT
- Austria
- Prior art keywords
- projectile
- missile
- self
- main motor
- propelled
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- 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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Air Bags (AREA)
- Toys (AREA)
- Automotive Seat Belt Assembly (AREA)
- Control Of Multiple Motors (AREA)
Abstract
The present invention relates to a self-propelled missile (10) of the type comprising an integrated main motor (40). According to the invention, the missile comprises, at the rear of the main motor (40), on the one hand a wing (28) intended for receiving an auxiliary motor (100) freely in terms of translational movement parallel to the axis (12) of the missile, and on the other hand means (40) forming a stop limiting the displacement of the auxiliary motor (100) forwards in relation to the missile, in such a way that the auxiliary motor (100) propels the missile (10) in the initial phase of its trajectory, initiates the main motor (40) at the end of its active phase and is then expelled rearwards during the activation of the main motor (40). <IMAGE>
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8705116A FR2613824B1 (en) | 1987-04-10 | 1987-04-10 | SELF-PROPELLED ROCKET AND PYROTECHNIC LAUNCHING DEVICE INCORPORATING THE SAME |
EP88400829A EP0295970B1 (en) | 1987-04-10 | 1988-04-06 | Self-propelled missile and launcher with a pyrotechnical ignition device for carrying such a missile |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE78335T1 true ATE78335T1 (en) | 1992-08-15 |
Family
ID=9350008
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT88400829T ATE78335T1 (en) | 1987-04-10 | 1988-04-06 | SELF-PROPELLED PROJECTILE AND A LAUNCHING DEVICE EQUIPPED WITH A PYROTECHNIC IGNITION SYSTEM, INCLUDING SUCH A PROJECTILE. |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0295970B1 (en) |
AT (1) | ATE78335T1 (en) |
DE (1) | DE3872773T2 (en) |
ES (1) | ES2034293T3 (en) |
FR (1) | FR2613824B1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19828645C1 (en) | 1998-06-26 | 1999-11-18 | Buck Werke Gmbh & Co I K | Guided missile for fixed or moving targets |
CN105333775B (en) * | 2015-11-30 | 2017-08-25 | 航宇救生装备有限公司 | The bindiny mechanism of rotating parachute and body |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE682694C (en) * | 1935-03-09 | 1939-10-20 | Louis Damblanc | Sling rocket |
FR854391A (en) * | 1938-12-31 | 1940-04-11 | Jet propelled machine | |
DE1099804B (en) * | 1957-12-31 | 1961-02-16 | Heinrich Klein Dr Ing | Two-stage rocket with a combustible base stage |
FR1252630A (en) * | 1959-06-11 | 1961-02-03 | Flying machine | |
US3190221A (en) * | 1961-12-27 | 1965-06-22 | John M Gariboldi | Rocket stage coupling |
FR1394264A (en) * | 1964-02-21 | 1965-04-02 | Ruggieri Ets | Self-propelled rocket with fins |
FR1546763A (en) * | 1967-10-12 | 1968-11-22 | Ruggieri Ets | Self-propelled pyrotechnic device and composition for its propulsion |
FR2376300A1 (en) * | 1976-12-28 | 1978-07-28 | Luchaire Sa | DEVICE FOR THE CONNECTION BETWEEN TWO STAGES OF A SELF-PROPELLED MACHINE |
-
1987
- 1987-04-10 FR FR8705116A patent/FR2613824B1/en not_active Expired - Fee Related
-
1988
- 1988-04-06 DE DE8888400829T patent/DE3872773T2/en not_active Expired - Fee Related
- 1988-04-06 ES ES198888400829T patent/ES2034293T3/en not_active Expired - Lifetime
- 1988-04-06 AT AT88400829T patent/ATE78335T1/en not_active IP Right Cessation
- 1988-04-06 EP EP88400829A patent/EP0295970B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2613824A1 (en) | 1988-10-14 |
FR2613824B1 (en) | 1993-05-28 |
EP0295970A1 (en) | 1988-12-21 |
ES2034293T3 (en) | 1993-04-01 |
EP0295970B1 (en) | 1992-07-15 |
DE3872773D1 (en) | 1992-08-20 |
DE3872773T2 (en) | 1993-02-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |