FR2231947B1 - - Google Patents

Info

Publication number
FR2231947B1
FR2231947B1 FR7320013A FR7320013A FR2231947B1 FR 2231947 B1 FR2231947 B1 FR 2231947B1 FR 7320013 A FR7320013 A FR 7320013A FR 7320013 A FR7320013 A FR 7320013A FR 2231947 B1 FR2231947 B1 FR 2231947B1
Authority
FR
France
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
Application number
FR7320013A
Other languages
French (fr)
Other versions
FR2231947A1 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Societe dEtudes de Realisations et dApplications Techniques SA SERAT
Original Assignee
Societe dEtudes de Realisations et dApplications Techniques SA SERAT
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Societe dEtudes de Realisations et dApplications Techniques SA SERAT filed Critical Societe dEtudes de Realisations et dApplications Techniques SA SERAT
Priority to FR7320013A priority Critical patent/FR2231947A1/fr
Publication of FR2231947A1 publication Critical patent/FR2231947A1/fr
Application granted granted Critical
Publication of FR2231947B1 publication Critical patent/FR2231947B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/665Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/222Homing guidance systems for spin-stabilized missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/663Steering 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)
FR7320013A 1973-06-01 1973-06-01 Rocket guidance system - clock device actuates pulse type target dector and course controller Granted FR2231947A1 (en)

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 FR2231947A1 (en) 1974-12-27
FR2231947B1 true 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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4408735A (en) 1979-11-09 1983-10-11 Thomson-Csf Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing this process

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE429064B (sv) * 1976-04-02 1983-08-08 Bofors Ab Slutfaskorrigering av roterande projektil
FR2401400A1 (fr) * 1977-08-23 1979-03-23 Serat Arme antichar sol-sol
US10514240B1 (en) 1981-10-02 2019-12-24 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
SE456036B (sv) * 1983-07-05 1988-08-29 Bofors Ab Sett och anordning for att styra en ur en kanon utskjutbar projektil mot ett mal

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1201401A (fr) * 1946-04-19 1959-12-30 Engin autodirigé
NL228838A (enrdf_load_stackoverflow) * 1957-06-19
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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4408735A (en) 1979-11-09 1983-10-11 Thomson-Csf Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing this process

Also Published As

Publication number Publication date
FR2231947A1 (en) 1974-12-27

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Legal Events

Date Code Title Description
ST Notification of lapse