SE8600812D0 - Flugkorper mit uberkalibrigem leitwerk - Google Patents

Flugkorper mit uberkalibrigem leitwerk

Info

Publication number
SE8600812D0
SE8600812D0 SE8600812A SE8600812A SE8600812D0 SE 8600812 D0 SE8600812 D0 SE 8600812D0 SE 8600812 A SE8600812 A SE 8600812A SE 8600812 A SE8600812 A SE 8600812A SE 8600812 D0 SE8600812 D0 SE 8600812D0
Authority
SE
Sweden
Prior art keywords
projectile
guidance
control surfaces
firing
barrel
Prior art date
Application number
SE8600812A
Other languages
English (en)
Other versions
SE8600812L (sv
Inventor
B Brieseck
J Nagler
Original Assignee
Diehl Gmbh & Co
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 Diehl Gmbh & Co filed Critical Diehl Gmbh & Co
Publication of SE8600812D0 publication Critical patent/SE8600812D0/sv
Publication of SE8600812L publication Critical patent/SE8600812L/sv

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
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Mold Materials And Core Materials (AREA)
  • Polysaccharides And Polysaccharide Derivatives (AREA)
SE8600812A 1985-03-05 1986-02-24 Flygkropp med overkalibrigt rodersystem SE8600812L (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853507677 DE3507677A1 (de) 1985-03-05 1985-03-05 Flugkoerper mit ueberkalibrigem leitwerk

Publications (2)

Publication Number Publication Date
SE8600812D0 true SE8600812D0 (sv) 1986-02-24
SE8600812L SE8600812L (sv) 1986-09-06

Family

ID=6264197

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8600812A SE8600812L (sv) 1985-03-05 1986-02-24 Flygkropp med overkalibrigt rodersystem

Country Status (6)

Country Link
US (1) US4728058A (sv)
JP (1) JPS61208499A (sv)
DE (1) DE3507677A1 (sv)
FR (1) FR2578640B1 (sv)
GB (1) GB2194838B (sv)
SE (1) SE8600812L (sv)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3721512C1 (de) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Flugkoerper mit ueberkalibrigem Leitwerk
DE4119613C2 (de) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Flugkörper mit ausklappbaren Leiteinrichtungen
DE4335785A1 (de) * 1993-10-20 1995-04-27 Diehl Gmbh & Co Ruderstelleinrichtung
DE19827278A1 (de) * 1998-06-19 1999-12-23 Diehl Stiftung & Co Lenkbarer Flugkörper
DE19827277B4 (de) * 1998-06-19 2006-08-10 Diehl Stiftung & Co.Kg Lageranordnung für die aufschwenkbaren Ruderblätter eines lenkbaren Flugkörpers
US6352217B1 (en) 2000-04-25 2002-03-05 Hr Textron, Inc. Missile fin locking and unlocking mechanism including a mechanical force amplifier
DE10118216A1 (de) 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Ruderblatt-Lagereinrichtung für ein Geschoß
DE10162136B4 (de) 2001-12-18 2004-10-14 Diehl Munitionssysteme Gmbh & Co. Kg Aus einem Rohr zu verschießender Flugkörper mit überkalibrigem Leitwerk
DE10205043C5 (de) 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg Aus einem Rohr zu verschließender Flugkörper mit überkalibrigem Leitwerk
FR2860577B1 (fr) * 2003-10-06 2006-01-27 Giat Ind Sa Dispositif de deploiement d'une ailette d'un projectile
FR2864612B1 (fr) * 2003-12-24 2007-11-23 Giat Ind Sa Dispositif de deploiement des ailettes d'un projectile
FR2895071B1 (fr) * 2005-12-19 2008-01-18 Giat Ind Sa Dispositif de verrouillage anti-rebond d'une ailette deployable d'un projectile.
DE102008007432A1 (de) * 2008-02-01 2009-08-06 Deutsch Französisches Forschungsinstitut Saint Louis Drallstabilisiertes Geschoss mit Leitflügeln
IL189785A (en) * 2008-02-26 2013-07-31 Elbit Systems Ltd Foldable and layout board
US8278612B2 (en) * 2010-07-27 2012-10-02 Raytheon Company Aerodynamic fin lock for adjustable and deployable fin
IL214191A (en) * 2011-07-19 2017-06-29 Elkayam Ami Ammunition guidance system and method for assembly
RU2482433C1 (ru) * 2011-12-07 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Раскрываемое крыло двухступенчатой ракеты
RU2482434C1 (ru) * 2011-12-14 2013-05-20 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Раскрываемое крыло двухступенчатой ракеты
RU2652035C1 (ru) * 2016-12-19 2018-04-24 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Механизм раскрытия консолей крыла летательного аппарата
RU185462U1 (ru) * 2018-02-15 2018-12-07 Общество с ограниченной ответственностью НАУЧНО-ПРОИЗВОДСТВЕННОЕ ОБЪЕДИНЕНИЕ "ЦЕЛЬ" Узел раскрытия аэродинамических поверхностей летательных аппаратов

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB577651A (en) * 1944-04-05 1946-05-27 Gilbert Henry Rye Williams Improvements in or relating to bomb tails
GB807561A (en) * 1956-03-12 1959-01-14 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
FR1405380A (fr) * 1964-05-28 1965-07-09 Soc Tech De Rech Ind Perfectionnements aux empennages déployants pour projectiles
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
US3415467A (en) * 1967-01-30 1968-12-10 Joseph A. Barringer Retrievable rocket with folded wings
CH480612A (de) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rakete mit Klappleitwerk und Bremsvorrichtung
CH481364A (de) * 1967-09-21 1969-11-15 Oerlikon Buehrle Ag Rakete mit aufklappbarem Leitwerk
US3643599A (en) * 1968-07-22 1972-02-22 Us Navy Retractable stabilizer fins and drag brakes for missiles
CH527405A (fr) * 1970-07-10 1972-08-31 Sarmac Sa Ensemble comprenant un projectile autopropulsé empenné et son étui
US3695556A (en) * 1970-08-03 1972-10-03 Us Navy Hinged stability and control fin assembly
DE2227104C2 (de) * 1972-06-03 1982-07-15 Dynamit Nobel Ag, 5210 Troisdorf Geschoß oder Rakete mit aufklappbarem Leitwerk
US3790104A (en) * 1973-03-12 1974-02-05 Us Navy High/low aspect ratio dual-mode fin design
DE2558060C2 (de) * 1975-12-22 1986-01-23 Rheinmetall GmbH, 4000 Düsseldorf Trägergeschoß für ausstoßbare Körper
DE2623582C2 (de) * 1976-05-26 1985-06-13 Rheinmetall GmbH, 4000 Düsseldorf Raketengeschoß mit Ausklappleitwerk und Treibspiegel
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
DE3048941A1 (de) * 1980-12-24 1982-07-15 Dynamit Nobel Ag, 5210 Troisdorf Leitwerk fuer aus einem rohr abzufeuernde flugkoerper, insbesondere grananten
DE3304913A1 (de) * 1982-01-28 1984-11-29 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk fuer ein ke-geschoss
DE3222378A1 (de) * 1982-06-15 1983-12-15 Dynamit Nobel Ag, 5210 Troisdorf Vorrichtung zur verringerung der empfindlichkeit leitwerksstabilisierter, in luft und/oder wasser sich bewegender gefechtskoerper gegen seitliche anstroemung
DE3432614A1 (de) * 1984-09-05 1986-03-13 Rheinmetall GmbH, 4000 Düsseldorf Flugkoerper
DE3434879A1 (de) * 1984-09-22 1986-04-03 Rheinmetall GmbH, 4000 Düsseldorf Arretierungsmittel fuer schwenkleitwerke von rohrmunition
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers

Also Published As

Publication number Publication date
GB2194838B (en) 1990-01-10
JPS61208499A (ja) 1986-09-16
SE8600812L (sv) 1986-09-06
GB8621232D0 (en) 1986-10-08
DE3507677A1 (de) 1986-09-11
FR2578640B1 (fr) 1990-08-31
GB2194838A (en) 1988-03-16
US4728058A (en) 1988-03-01
FR2578640A1 (fr) 1986-09-12
DE3507677C2 (sv) 1993-06-03

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Legal Events

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NAV Patent application has lapsed

Ref document number: 8600812-5

Effective date: 19920901