GB1431619A - Tube launched projectiles - Google Patents

Tube launched projectiles

Info

Publication number
GB1431619A
GB1431619A GB3345674A GB3345674A GB1431619A GB 1431619 A GB1431619 A GB 1431619A GB 3345674 A GB3345674 A GB 3345674A GB 3345674 A GB3345674 A GB 3345674A GB 1431619 A GB1431619 A GB 1431619A
Authority
GB
United Kingdom
Prior art keywords
projectile
fins
fin
tube
launched projectiles
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
Application number
GB3345674A
Other languages
English (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.)
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 GB1431619A publication Critical patent/GB1431619A/en
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)
GB3345674A 1973-08-24 1974-07-29 Tube launched projectiles Expired GB1431619A (en)

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 (1)

Publication Number Publication Date
GB1431619A true GB1431619A (en) 1976-04-14

Family

ID=5890609

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3345674A Expired GB1431619A (en) 1973-08-24 1974-07-29 Tube launched projectiles

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)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0202734A1 (de) * 1985-03-23 1986-11-26 British Aerospace Public Limited Company Vorrichtung zum Ausfahren von Flossen
EP0296735A2 (de) * 1987-06-26 1988-12-28 Hughes Aircraft Company Strömungsteilerplatte zur Verringerung des Luftwiderstandes von Flugkörperbefestigungsvorrichtungen

Families Citing this family (31)

* 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
US4709878A (en) * 1984-04-17 1987-12-01 British Aerospace Plc Fin assembly deployment spring
EP0248123B1 (de) * 1986-03-14 1988-09-28 British Aerospace Public Limited Company Feder für ausfahrbare Flächen
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
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
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
DE19941556C2 (de) * 1999-09-01 2001-07-12 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.
WO2011126970A2 (en) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
US8686329B2 (en) 2010-04-09 2014-04-01 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

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0202734A1 (de) * 1985-03-23 1986-11-26 British Aerospace Public Limited Company Vorrichtung zum Ausfahren von Flossen
US4714216A (en) * 1985-03-23 1987-12-22 British Aerospace Public Limited Company Fin erecting mechanisms
EP0296735A2 (de) * 1987-06-26 1988-12-28 Hughes Aircraft Company Strömungsteilerplatte zur Verringerung des Luftwiderstandes von Flugkörperbefestigungsvorrichtungen
EP0296735A3 (en) * 1987-06-26 1990-10-24 Hughes Aircraft Company Splitter plates for alleviation of missile hook drag

Also Published As

Publication number Publication date
SE7409982L (de) 1975-02-25
DE2342783C2 (de) 1983-12-22
FR2241761B3 (de) 1977-07-01
FR2241761A1 (de) 1975-03-21
US3918664A (en) 1975-11-11
DE2342783A1 (de) 1975-03-06

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee