GB1296346A - - Google Patents

Info

Publication number
GB1296346A
GB1296346A GB1296346DA GB1296346A GB 1296346 A GB1296346 A GB 1296346A GB 1296346D A GB1296346D A GB 1296346DA GB 1296346 A GB1296346 A GB 1296346A
Authority
GB
United Kingdom
Prior art keywords
fins
launching
projectile
feb
cone
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
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 filed Critical
Publication of GB1296346A publication Critical patent/GB1296346A/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
    • 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)

Abstract

1296346 Fins MESSERSCHMITT-BOLKOW-BLOHM GmbH 3 Feb 1970 [7 Feb 1969] 5040/70 Heading F3A] A projectile for launching from a tube comprises fins 17 which, on launching, are pushed by a spring 12 along the surface of a cone 7 into an extended position. The fins are guided by slots 20 in the projectile casing and are arranged to be both frictionally and positively secured in the extended position. Prior to launching arcuate portions 19 of the fins bear against the inside surface of the launching tube to secure them in a retracted position. As the fins move they also operate a timing mechanism for a detonator. The cone 7 can be used for accomodating a jet propulsion unit or the tip of a corresponding projectile.
GB1296346D 1969-02-07 1970-02-03 Expired GB1296346A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1906028A DE1906028C3 (en) 1969-02-07 1969-02-07 Tail unit for projectiles and missiles with a device for moving the fins of the tail unit into their effective position

Publications (1)

Publication Number Publication Date
GB1296346A true GB1296346A (en) 1972-11-15

Family

ID=5724558

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1296346D Expired GB1296346A (en) 1969-02-07 1970-02-03

Country Status (4)

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

Families Citing this family (13)

* 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
DE2264338A1 (en) * 1972-12-30 1974-07-04 Dynamit Nobel Ag FOLD-OUT TAIL, ESPECIALLY FOR MISSILE
US3819132A (en) * 1973-02-21 1974-06-25 Sarmac Sa Self propelled projectile with fins
DE3933100A1 (en) * 1988-12-19 1990-06-28 Diehl Gmbh & Co CONTROL UNIT FOR A SUB-CALIBRATE ARROW FLOOR
US5398887A (en) * 1993-10-12 1995-03-21 Thiokol Corporation Finless aerodynamic control system
DE4434769A1 (en) * 1994-09-29 1996-04-04 Friedrich Von Rohrscheidt Ring comb binder mfd. by injection moulding, to hold stacked sheets of paper
US5697721A (en) * 1996-05-31 1997-12-16 Von Rohrscheidt; Friedrich Injection moldable sheet binder
DE19712596A1 (en) * 1997-03-26 1998-10-01 Friedrich Von Rohrscheidt Back binding for binding leaves
US6761331B2 (en) * 2002-03-19 2004-07-13 Raytheon Company Missile having deployment mechanism for stowable fins
DE10337973B4 (en) * 2003-08-19 2005-11-17 Eads Space Transportation Gmbh Ejection device for spin-stabilized spacecraft
DE102004063116B3 (en) * 2004-12-23 2006-04-27 Eads Space Transportation Gmbh Missile ejection device for space craft, has ring units and twisted towing ropes arranged between ring units, and missile holding and guiding units arranged at ring unit connected with structure of space craft
DE102004063115B3 (en) * 2004-12-23 2006-05-04 Eads Space Transportation Gmbh Spin-stabilized vessel dropping device for spacecraft, has central rope roll placed on ring which serves as holding ring, in which vessel is set in translatory motion when vessel, placed on holding ring, rotates along with holding ring
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 (en) * 1921-12-23 1923-07-17 Improvements to tail projectiles
DE1553980C3 (en) * 1965-02-18 1975-05-22 Breda Meccanica Bresciana S.P.A., Brescia (Italien) Device for adjusting the firing range of rocket projectiles

Also Published As

Publication number Publication date
DE1906028B2 (en) 1973-05-17
FR2033805A5 (en) 1970-12-04
DE1906028C3 (en) 1973-12-06
DE1906028A1 (en) 1970-08-20
US3684214A (en) 1972-08-15

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees