FR2033805A5 - - Google Patents

Info

Publication number
FR2033805A5
FR2033805A5 FR7003439A FR7003439A FR2033805A5 FR 2033805 A5 FR2033805 A5 FR 2033805A5 FR 7003439 A FR7003439 A FR 7003439A FR 7003439 A FR7003439 A FR 7003439A FR 2033805 A5 FR2033805 A5 FR 2033805A5
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
FR7003439A
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Application granted granted Critical
Publication of FR2033805A5 publication Critical patent/FR2033805A5/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
    • F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
FR7003439A 1969-02-07 1970-01-30 Expired FR2033805A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1906028A DE1906028C3 (de) 1969-02-07 1969-02-07 Leitwerk fur Geschosse und Flug korper mit einer Einrichtung zur Über fuhrung der Flossen des Leitwerkes in ihre wirksame Stellung

Publications (1)

Publication Number Publication Date
FR2033805A5 true FR2033805A5 (fr) 1970-12-04

Family

ID=5724558

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7003439A Expired FR2033805A5 (fr) 1969-02-07 1970-01-30

Country Status (4)

Country Link
US (1) US3684214A (fr)
DE (1) DE1906028C3 (fr)
FR (1) FR2033805A5 (fr)
GB (1) GB1296346A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2212528A1 (fr) * 1972-12-30 1974-07-26 Dynamit Nobel Ag

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1103353A (en) * 1965-11-18 1968-02-14 Charles John Broadhurst Improvements in fitments for loose leaf binders
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
DE3933100A1 (de) * 1988-12-19 1990-06-28 Diehl Gmbh & Co Leitwerk fuer ein unterkalibriges uebungspfeilgeschoss
US5398887A (en) * 1993-10-12 1995-03-21 Thiokol Corporation Finless aerodynamic control system
DE4434769A1 (de) * 1994-09-29 1996-04-04 Friedrich Von Rohrscheidt Binderücken
US5697721A (en) * 1996-05-31 1997-12-16 Von Rohrscheidt; Friedrich Injection moldable sheet binder
DE19712596A1 (de) * 1997-03-26 1998-10-01 Friedrich Von Rohrscheidt Binderücken zum Binden von Blättern
US6761331B2 (en) * 2002-03-19 2004-07-13 Raytheon Company Missile having deployment mechanism for stowable fins
DE10337973B4 (de) * 2003-08-19 2005-11-17 Eads Space Transportation Gmbh Auswurfvorrichtung für drallstabilisierte Raumflugkörper
DE102004063115B3 (de) * 2004-12-23 2006-05-04 Eads Space Transportation Gmbh Auswurfvorrichtung für drallstabilisierte Behälter
DE102004063116B3 (de) * 2004-12-23 2006-04-27 Eads Space Transportation Gmbh Auswurfvorrichtung für drallstabilisierte Behälter
US7642492B2 (en) * 2005-01-26 2010-01-05 Raytheon Company Single-axis fin deployment system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR556302A (fr) * 1921-12-23 1923-07-17 Perfectionnements aux projectiles à empennage
DE1553980C3 (de) * 1965-02-18 1975-05-22 Breda Meccanica Bresciana S.P.A., Brescia (Italien) Vorrichtung zum Einstellen der Schußweite von Raketengeschossen

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2212528A1 (fr) * 1972-12-30 1974-07-26 Dynamit Nobel Ag

Also Published As

Publication number Publication date
DE1906028A1 (de) 1970-08-20
US3684214A (en) 1972-08-15
DE1906028C3 (de) 1973-12-06
GB1296346A (fr) 1972-11-15
DE1906028B2 (de) 1973-05-17

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Legal Events

Date Code Title Description
ST Notification of lapse