IL35877A - Projectile with separable body having rotational braking means - Google Patents

Projectile with separable body having rotational braking means

Info

Publication number
IL35877A
IL35877A IL35877A IL3587770A IL35877A IL 35877 A IL35877 A IL 35877A IL 35877 A IL35877 A IL 35877A IL 3587770 A IL3587770 A IL 3587770A IL 35877 A IL35877 A IL 35877A
Authority
IL
Israel
Prior art keywords
projectile
braking means
rotational braking
separable body
separable
Prior art date
Application number
IL35877A
Other versions
IL35877A0 (en
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Publication of IL35877A0 publication Critical patent/IL35877A0/en
Publication of IL35877A publication Critical patent/IL35877A/en

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
    • F42B10/16—Wrap-around fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
IL35877A 1970-01-08 1970-12-18 Projectile with separable body having rotational braking means IL35877A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE00147/70A SE339646B (en) 1970-01-08 1970-01-08

Publications (2)

Publication Number Publication Date
IL35877A0 IL35877A0 (en) 1971-04-28
IL35877A true IL35877A (en) 1974-05-16

Family

ID=20256110

Family Applications (1)

Application Number Title Priority Date Filing Date
IL35877A IL35877A (en) 1970-01-08 1970-12-18 Projectile with separable body having rotational braking means

Country Status (7)

Country Link
US (1) US3702588A (en)
DE (1) DE2100489C3 (en)
FR (1) FR2075263A5 (en)
GB (1) GB1304671A (en)
IL (1) IL35877A (en)
NL (1) NL7100151A (en)
SE (1) SE339646B (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE353956B (en) * 1971-06-24 1973-02-19 Bofors Ab
US3834312A (en) * 1973-03-14 1974-09-10 Bofors Ab Parachute-borne flare assemblage
FR2260772B1 (en) * 1974-02-08 1976-06-25 France Etat
DE2518645C2 (en) * 1975-04-26 1986-07-17 Rheinmetall GmbH, 4000 Düsseldorf Twist brake for a payload that can be ejected from a twist projectile
US4004514A (en) * 1976-01-20 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Roll rate stabilized wrap around missile fins
SE416235B (en) * 1976-12-27 1980-12-08 Bofors Ab BRAKE DEVICE FOR ROTATING BODY
IL63885A (en) * 1981-09-20 1988-04-29 Aryeh Ashkenazi Telescopic projectile and apparatus for firing same
DE3422231A1 (en) * 1984-06-15 1985-12-19 Diehl GmbH & Co, 8500 Nürnberg DEVICE FOR AERODYNAMICALLY BRAKING THE ROTATIONAL MOVEMENT OF A BODY
DE3435420A1 (en) * 1984-09-27 1986-04-03 Rheinmetall GmbH, 4000 Düsseldorf SKULL HEAD
NL192056C (en) * 1985-03-12 1997-01-07 Eurometaal Nv Cylindrical metal holder with rotation brake flaps.
GB8609166D0 (en) * 1986-04-15 1986-09-17 British Aerospace Deployment arrangement for spinning body
SE460436B (en) * 1986-12-01 1989-10-09 Bofors Ab DEVICE TO REDUCE ROTATION AND AT THE SAME TIME GET A SIDE SPEED OF A ROTATING AMMUNITION UNIT
GB9015445D0 (en) * 1990-07-13 1991-02-20 Royal Ordnance Plc Projectile surveillance apparatus
US5117731A (en) * 1991-11-04 1992-06-02 The United States Of America As Represented By The Secretary Of The Navy Tactical acoustic decoy
CH685069A5 (en) * 1991-12-18 1995-03-15 Contraves Ag Sub-calibre, fin-stabilised projectile which is fired with spin
SE508858C2 (en) * 1997-03-25 1998-11-09 Bofors Ab Fine stabilized grenade
SE508857C2 (en) * 1997-03-25 1998-11-09 Bofors Ab Fine stabilized base bleed grenade
SE518665C2 (en) * 2000-03-21 2002-11-05 Bofors Weapon Sys Ab Fine stabilized artillery grenade
SE521445C2 (en) 2001-03-20 2003-11-04 Bofors Defence Ab Methods for synchronizing the fine precipitation in a finely stabilized artillery grenade and a correspondingly designed artillery grenade
US6745978B1 (en) * 2003-03-24 2004-06-08 At&T Corp. Aerodynamic stabilization of a projectile
US6783095B1 (en) 2003-03-24 2004-08-31 At&T Corp. Deployable flare for aerodynamically stabilizing a projectile
DE102005026070B4 (en) * 2005-06-07 2009-07-09 Diehl Bgt Defence Gmbh & Co. Kg Wing arrangement and missile
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
IL231186A (en) * 2014-02-26 2017-07-31 Israel Aerospace Ind Ltd Fin deployment system
SE540780C2 (en) * 2016-04-06 2018-11-06 Bae Systems Bofors Ab Divisible grenade with parachute
US10466023B2 (en) * 2018-03-28 2019-11-05 Ascendance International, LLC Long range large caliber frangible round for defending against UAV'S
DE102021005973A1 (en) 2021-12-03 2023-06-07 Diehl Defence Gmbh & Co. Kg Projectile with fins that can be swung out without springs

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US17407A (en) * 1857-05-26 Improved projectile for killing whales
US617376A (en) * 1899-01-10 Railroad signal-fusee
US2599703A (en) * 1949-09-02 1952-06-10 Bendix Aviat Corp Lockout warning system for home heating apparatus
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
US3578796A (en) * 1968-09-25 1971-05-18 Thiokol Chemical Corp Spinning and stabilizing system for solid propellant rocket or missiles

Also Published As

Publication number Publication date
DE2100489B2 (en) 1974-11-28
US3702588A (en) 1972-11-14
DE2100489A1 (en) 1971-07-15
NL7100151A (en) 1971-07-12
SE339646B (en) 1971-10-11
GB1304671A (en) 1973-01-24
IL35877A0 (en) 1971-04-28
FR2075263A5 (en) 1971-10-08
DE2100489C3 (en) 1975-07-17

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