FR2231947A1 - Rocket guidance system - clock device actuates pulse type target dector and course controller - Google Patents
Rocket guidance system - clock device actuates pulse type target dector and course controllerInfo
- Publication number
- FR2231947A1 FR2231947A1 FR7320013A FR7320013A FR2231947A1 FR 2231947 A1 FR2231947 A1 FR 2231947A1 FR 7320013 A FR7320013 A FR 7320013A FR 7320013 A FR7320013 A FR 7320013A FR 2231947 A1 FR2231947 A1 FR 2231947A1
- Authority
- FR
- France
- Prior art keywords
- rocket
- clock device
- dector
- guidance system
- course
- 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.)
- Granted
Links
- 238000001514 detection method Methods 0.000 abstract 3
- 239000002360 explosive Substances 0.000 abstract 1
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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/222—Homing guidance systems for spin-stabilized missiles
-
- 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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7320013A FR2231947A1 (en) | 1973-06-01 | 1973-06-01 | Rocket guidance system - clock device actuates pulse type target dector and course controller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7320013A FR2231947A1 (en) | 1973-06-01 | 1973-06-01 | Rocket guidance system - clock device actuates pulse type target dector and course controller |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2231947A1 true FR2231947A1 (en) | 1974-12-27 |
FR2231947B1 FR2231947B1 (enrdf_load_stackoverflow) | 1977-05-06 |
Family
ID=9120382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7320013A Granted FR2231947A1 (en) | 1973-06-01 | 1973-06-01 | Rocket guidance system - clock device actuates pulse type target dector and course controller |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2231947A1 (enrdf_load_stackoverflow) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2346673A1 (fr) * | 1976-04-02 | 1977-10-28 | Bofors Ab | Dispositif de correction de la trajectoire d'un projectile |
FR2401400A1 (fr) * | 1977-08-23 | 1979-03-23 | Serat | Arme antichar sol-sol |
EP0028966A1 (fr) * | 1979-11-09 | 1981-05-20 | Thomson-Brandt Armements | Procédé de pilotage et de guidage de projectiles en phase terminale de vol |
FR2517818A1 (fr) * | 1981-12-09 | 1983-06-10 | Thomson Brandt | Methode de guidage terminal et missile guide operant selon cette methode |
FR2548774A1 (fr) * | 1983-07-05 | 1985-01-11 | Bofors Ab | Projectile lance par un canon et muni d'un radar, et procede de reglage de la trajectoire d'un tel projectile |
US10514240B1 (en) | 1981-10-02 | 2019-12-24 | The Boeing Company | Multiple wire guided submissile target assignment logic |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1194707A (fr) * | 1957-06-19 | 1959-11-12 | Eltro Gmbh | Appareil de guidage final pour fusées de petit calibre, en particulier |
FR1201401A (fr) * | 1946-04-19 | 1959-12-30 | Engin autodirigé | |
US3072365A (en) * | 1957-09-16 | 1963-01-08 | Missile Corp | Pilotless craft guidance method and means |
GB1025740A (en) * | 1964-12-18 | 1966-04-14 | William Burdette Mclean | Proportional navigation system for a spinning body in free space |
US3712562A (en) * | 1964-05-19 | 1973-01-23 | Us Navy | Sector gating circuit |
-
1973
- 1973-06-01 FR FR7320013A patent/FR2231947A1/fr active Granted
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1201401A (fr) * | 1946-04-19 | 1959-12-30 | Engin autodirigé | |
FR1194707A (fr) * | 1957-06-19 | 1959-11-12 | Eltro Gmbh | Appareil de guidage final pour fusées de petit calibre, en particulier |
US3072365A (en) * | 1957-09-16 | 1963-01-08 | Missile Corp | Pilotless craft guidance method and means |
US3712562A (en) * | 1964-05-19 | 1973-01-23 | Us Navy | Sector gating circuit |
GB1025740A (en) * | 1964-12-18 | 1966-04-14 | William Burdette Mclean | Proportional navigation system for a spinning body in free space |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2346673A1 (fr) * | 1976-04-02 | 1977-10-28 | Bofors Ab | Dispositif de correction de la trajectoire d'un projectile |
FR2401400A1 (fr) * | 1977-08-23 | 1979-03-23 | Serat | Arme antichar sol-sol |
EP0028966A1 (fr) * | 1979-11-09 | 1981-05-20 | Thomson-Brandt Armements | Procédé de pilotage et de guidage de projectiles en phase terminale de vol |
US10514240B1 (en) | 1981-10-02 | 2019-12-24 | The Boeing Company | Multiple wire guided submissile target assignment logic |
USRE49911E1 (en) | 1981-10-02 | 2024-04-09 | The Boeing Company | Multiple wire guided submissile target assignment logic |
FR2517818A1 (fr) * | 1981-12-09 | 1983-06-10 | Thomson Brandt | Methode de guidage terminal et missile guide operant selon cette methode |
EP0081421A1 (fr) * | 1981-12-09 | 1983-06-15 | Thomson-Brandt Armements | Méthode de guidage terminal et missile guidé opérant selon cette méthode |
US4568040A (en) * | 1981-12-09 | 1986-02-04 | Thomson-Brandt | Terminal guidance method and a guided missile operating according to this method |
FR2548774A1 (fr) * | 1983-07-05 | 1985-01-11 | Bofors Ab | Projectile lance par un canon et muni d'un radar, et procede de reglage de la trajectoire d'un tel projectile |
US4679748A (en) * | 1983-07-05 | 1987-07-14 | Ake Blomqvist | Cannon-launched projectile scanner |
Also Published As
Publication number | Publication date |
---|---|
FR2231947B1 (enrdf_load_stackoverflow) | 1977-05-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |