FR2613824B1 - SELF-PROPELLED ROCKET AND PYROTECHNIC LAUNCHING DEVICE INCORPORATING THE SAME - Google Patents

SELF-PROPELLED ROCKET AND PYROTECHNIC LAUNCHING DEVICE INCORPORATING THE SAME

Info

Publication number
FR2613824B1
FR2613824B1 FR8705116A FR8705116A FR2613824B1 FR 2613824 B1 FR2613824 B1 FR 2613824B1 FR 8705116 A FR8705116 A FR 8705116A FR 8705116 A FR8705116 A FR 8705116A FR 2613824 B1 FR2613824 B1 FR 2613824B1
Authority
FR
France
Prior art keywords
missile
self
main motor
same
launching device
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 - Fee Related
Application number
FR8705116A
Other languages
French (fr)
Other versions
FR2613824A1 (en
Inventor
Jean Baricos
Michel Castarede
Philippe Rousseau
Denis Dilhan
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.)
Etienne LaCroix Tous Artifices SA
Original Assignee
Etienne LaCroix Tous Artifices SA
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 Etienne LaCroix Tous Artifices SA filed Critical Etienne LaCroix Tous Artifices SA
Priority to FR8705116A priority Critical patent/FR2613824B1/en
Priority to DE8888400829T priority patent/DE3872773T2/en
Priority to AT88400829T priority patent/ATE78335T1/en
Priority to ES198888400829T priority patent/ES2034293T3/en
Priority to EP88400829A priority patent/EP0295970B1/en
Publication of FR2613824A1 publication Critical patent/FR2613824A1/en
Application granted granted Critical
Publication of FR2613824B1 publication Critical patent/FR2613824B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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)
  • Toys (AREA)
  • Air Bags (AREA)
  • Control Of Multiple Motors (AREA)
  • Automotive Seat Belt Assembly (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).
FR8705116A 1987-04-10 1987-04-10 SELF-PROPELLED ROCKET AND PYROTECHNIC LAUNCHING DEVICE INCORPORATING THE SAME Expired - Fee Related FR2613824B1 (en)

Priority Applications (5)

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
DE8888400829T DE3872773T2 (en) 1987-04-10 1988-04-06 SELF-DRIVEN BULLET AND A COMBUSTION DEVICE PROVIDED WITH A PYROTECHNICAL IGNITION SYSTEM THAT CONTAINS SUCH A BULLET.
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.
ES198888400829T ES2034293T3 (en) 1987-04-10 1988-04-06 SELF-PROPELLED PROJECTILE AND LAUNCH DEVICE, WHICH INCLUDES A PYROTECHNICAL IGNITION SYSTEM, WHICH INCORPORATES THIS PROJECTILE.
EP88400829A EP0295970B1 (en) 1987-04-10 1988-04-06 Self-propelled missile and launcher with a pyrotechnical ignition device for carrying such a missile

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2613824A1 FR2613824A1 (en) 1988-10-14
FR2613824B1 true FR2613824B1 (en) 1993-05-28

Family

ID=9350008

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8705116A Expired - Fee Related FR2613824B1 (en) 1987-04-10 1987-04-10 SELF-PROPELLED ROCKET AND PYROTECHNIC LAUNCHING DEVICE INCORPORATING THE SAME

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
EP0295970B1 (en) 1992-07-15
EP0295970A1 (en) 1988-12-21
ES2034293T3 (en) 1993-04-01
DE3872773D1 (en) 1992-08-20
DE3872773T2 (en) 1993-02-25
FR2613824A1 (en) 1988-10-14
ATE78335T1 (en) 1992-08-15

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20061230