FR2241761B3 - - Google Patents

Info

Publication number
FR2241761B3
FR2241761B3 FR7428945A FR7428945A FR2241761B3 FR 2241761 B3 FR2241761 B3 FR 2241761B3 FR 7428945 A FR7428945 A FR 7428945A FR 7428945 A FR7428945 A FR 7428945A FR 2241761 B3 FR2241761 B3 FR 2241761B3
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
FR7428945A
Other languages
French (fr)
Other versions
FR2241761A1 (de
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of FR2241761A1 publication Critical patent/FR2241761A1/fr
Application granted granted Critical
Publication of FR2241761B3 publication Critical patent/FR2241761B3/fr
Expired 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
    • 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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
FR7428945A 1973-08-24 1974-08-23 Expired FR2241761B3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2342783A DE2342783C2 (de) 1973-08-24 1973-08-24 Mit einem Leitwerk versehenes Geschoß

Publications (2)

Publication Number Publication Date
FR2241761A1 FR2241761A1 (de) 1975-03-21
FR2241761B3 true FR2241761B3 (de) 1977-07-01

Family

ID=5890609

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7428945A Expired FR2241761B3 (de) 1973-08-24 1974-08-23

Country Status (5)

Country Link
US (1) US3918664A (de)
DE (1) DE2342783C2 (de)
FR (1) FR2241761B3 (de)
GB (1) GB1431619A (de)
SE (1) SE7409982L (de)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
US4384691A (en) * 1980-12-22 1983-05-24 The United States Of America As Represented By The Secretary Of The Army Rocket fin hold down spring
US4588146A (en) * 1984-03-29 1986-05-13 The United States Of America As Represented By The Secretary Of The Army Biaxial folding lever wing
EP0248123B1 (de) * 1986-03-14 1988-09-28 British Aerospace Public Limited Company Feder für ausfahrbare Flächen
US4709878A (en) * 1984-04-17 1987-12-01 British Aerospace Plc Fin assembly deployment spring
DE3432614A1 (de) * 1984-09-05 1986-03-13 Rheinmetall GmbH, 4000 Düsseldorf Flugkoerper
DE3447852A1 (de) * 1984-12-31 1986-08-28 Heide, Marion, 4030 Ratingen Klappleitwerk fuer fluegelstabilisierte raketengeschosse
DE3664164D1 (en) * 1985-03-23 1989-08-03 British Aerospace Fin erecting mechanisms
US4809929A (en) * 1987-06-26 1989-03-07 Hughes Aircraft Company Splitter plates for alleviation of missile hook drag
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil
DE4016840A1 (de) * 1990-05-25 1991-11-28 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
DE4119613C2 (de) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Flugkörper mit ausklappbaren Leiteinrichtungen
SE9102702L (sv) * 1991-09-18 1993-03-19 Bofors Ab Stridsdel
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
FR2712679B1 (fr) * 1993-11-16 1996-02-09 Luchaire Defense Sa Dispositif de déploiement pour une ailette de stabilisation de projectile de type roquette.
IL107844A (en) * 1993-12-02 1996-06-18 Ministry Of Defence Armaments Flying object control system
DE19941556C2 (de) * 1999-09-01 2001-07-12 Rheinmetall W & M Gmbh Flugkörper
DE19941555C5 (de) * 1999-09-01 2004-12-30 Rheinmetall W & M Gmbh Flugkörper
DE19941557C5 (de) * 1999-09-01 2004-07-15 Rheinmetall W & M Gmbh Flugkörper
DE10118216A1 (de) * 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Ruderblatt-Lagereinrichtung für ein Geschoß
US6559370B1 (en) * 2002-08-06 2003-05-06 The United States Of America As Represented By The Secretary Of The Navy Submarine countermeasure vehicle with folding propeller
DE202005011174U1 (de) * 2005-07-15 2005-09-29 Glau, Felix Schussmunition
US7902489B2 (en) * 2007-12-17 2011-03-08 Raytheon Company Torsional spring aided control actuator for a rolling missile
US8338769B1 (en) * 2008-02-07 2012-12-25 Simmonds Precision Products, Inc. Pyrotechnic fin deployment and retention mechanism
FR2949848B1 (fr) 2009-09-10 2012-09-28 Nexter Munitions Dispositif d'ouverture et verrouillage d'une ailette canard.
US8754352B2 (en) * 2010-04-07 2014-06-17 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
WO2011127369A2 (en) * 2010-04-09 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Torsion spring wing deployment initiator
US8278612B2 (en) * 2010-07-27 2012-10-02 Raytheon Company Aerodynamic fin lock for adjustable and deployable fin
DE102015004702A1 (de) * 2014-12-11 2016-06-16 Mbda Deutschland Gmbh Rudersystem
RU2601889C1 (ru) * 2015-09-11 2016-11-10 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Вращающийся стабилизатор управляемой ракеты
CN109895987B (zh) * 2017-12-11 2021-06-18 中国科学院沈阳自动化研究所 一种海洋机器人用舵折叠装置
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE379532A (de) * 1930-05-22
CH302186A (fr) * 1952-10-06 1954-10-15 Energa Projectile empenné.
FR1191519A (fr) * 1958-02-13 1959-10-20 Hotchkiss Brandt Empennage déployant pour projectile d'artillerie
DE1578222A1 (de) * 1966-02-04 1972-02-10 Ind & Mecaniques S T R I M Sich entfaltendes Leitwerk,insbesondere fuer Raketen Societe Technique de Recherches
BE759788A (fr) * 1969-12-05 1971-06-03 Sarmac Sa Projectile autopropulse empenne
US3690595A (en) * 1970-11-19 1972-09-12 Sarmac Sa Self-propelled, vaned missile

Also Published As

Publication number Publication date
US3918664A (en) 1975-11-11
DE2342783A1 (de) 1975-03-06
FR2241761A1 (de) 1975-03-21
GB1431619A (en) 1976-04-14
SE7409982L (de) 1975-02-25
DE2342783C2 (de) 1983-12-22

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