CH480613A - Bullet with brake wings - Google Patents

Bullet with brake wings

Info

Publication number
CH480613A
CH480613A CH1266767A CH1266767A CH480613A CH 480613 A CH480613 A CH 480613A CH 1266767 A CH1266767 A CH 1266767A CH 1266767 A CH1266767 A CH 1266767A CH 480613 A CH480613 A CH 480613A
Authority
CH
Switzerland
Prior art keywords
bullet
brake wings
wings
brake
Prior art date
Application number
CH1266767A
Other languages
German (de)
Inventor
Suter Xaver
Original Assignee
Oerlikon Buehrle 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 Oerlikon Buehrle Ag filed Critical Oerlikon Buehrle Ag
Priority to CH1266767A priority Critical patent/CH480613A/en
Priority to FR1597485D priority patent/FR1597485A/fr
Priority to US755526A priority patent/US3588004A/en
Priority to SE11545/68A priority patent/SE352729B/xx
Priority to DE19681728140 priority patent/DE1728140B1/en
Priority to BE720312D priority patent/BE720312A/xx
Priority to AT848768A priority patent/AT283963B/en
Priority to JP43064700A priority patent/JPS4836800B1/ja
Priority to NL6812960A priority patent/NL6812960A/xx
Priority to GB43243/68A priority patent/GB1213505A/en
Publication of CH480613A publication Critical patent/CH480613A/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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Braking Arrangements (AREA)
  • Carbon And Carbon Compounds (AREA)
CH1266767A 1967-09-11 1967-09-11 Bullet with brake wings CH480613A (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
CH1266767A CH480613A (en) 1967-09-11 1967-09-11 Bullet with brake wings
FR1597485D FR1597485A (en) 1967-09-11 1968-08-26
US755526A US3588004A (en) 1967-09-11 1968-08-27 Missile with brake flaps
SE11545/68A SE352729B (en) 1967-09-11 1968-08-28
DE19681728140 DE1728140B1 (en) 1967-09-11 1968-08-30 Projectile with brake levers attached to a projectile body
BE720312D BE720312A (en) 1967-09-11 1968-09-02
AT848768A AT283963B (en) 1967-09-11 1968-09-02 Bullet with brake wings
JP43064700A JPS4836800B1 (en) 1967-09-11 1968-09-10
NL6812960A NL6812960A (en) 1967-09-11 1968-09-11
GB43243/68A GB1213505A (en) 1967-09-11 1968-09-11 Missile with brake flaps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1266767A CH480613A (en) 1967-09-11 1967-09-11 Bullet with brake wings

Publications (1)

Publication Number Publication Date
CH480613A true CH480613A (en) 1969-10-31

Family

ID=4385265

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1266767A CH480613A (en) 1967-09-11 1967-09-11 Bullet with brake wings

Country Status (10)

Country Link
US (1) US3588004A (en)
JP (1) JPS4836800B1 (en)
AT (1) AT283963B (en)
BE (1) BE720312A (en)
CH (1) CH480613A (en)
DE (1) DE1728140B1 (en)
FR (1) FR1597485A (en)
GB (1) GB1213505A (en)
NL (1) NL6812960A (en)
SE (1) SE352729B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4327886A (en) * 1972-11-30 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Integral rocket ramjet missile
GB1523963A (en) * 1976-02-26 1978-09-06 Hawker Siddeley Dynamics Ltd Method and means for auxiliary control of vehicle direction
US4295617A (en) * 1979-10-02 1981-10-20 The United States Of America As Represented By The Secretary Of The Army Selectable drag brakes for rocket range control
US4717093A (en) * 1985-08-12 1988-01-05 Grumman Aerospace Corporation Penguin missile folding wing configuration
US4691880A (en) * 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
FR2655722B1 (en) * 1989-12-12 1992-03-13 Aerospatiale SUPERSONIC MISSILE WITH TORQUE DRIVING BY SPOUILERS.
DE4119613C2 (en) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Missiles with fold-out guidance devices
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
US5762291A (en) * 1996-10-28 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Drag control module for stabilized projectiles
KR101234218B1 (en) 2010-06-25 2013-02-18 국방과학연구소 Wing device and flight vehicle having the same
GB2494203B (en) * 2011-09-05 2015-04-15 Michael Alculumbre Projectile
CN103389010B (en) * 2012-05-07 2015-07-22 刘应杰 Rocket projectile with vanes fixed in gapless manner and unstressed lug hinge pins on tail section
FR3041744B1 (en) * 2015-09-29 2018-08-17 Nexter Munitions ARTILLERY PROJECTILE HAVING A PILOTED PHASE.

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2465401A (en) * 1943-09-23 1949-03-29 Leslie A Skinner Rocket fin assembly
FR1191519A (en) * 1958-02-13 1959-10-20 Hotchkiss Brandt Deploying tail for artillery projectile
NL266892A (en) * 1960-07-11

Also Published As

Publication number Publication date
AT283963B (en) 1970-08-25
FR1597485A (en) 1970-06-29
SE352729B (en) 1973-01-08
NL6812960A (en) 1969-03-13
JPS4836800B1 (en) 1973-11-07
BE720312A (en) 1969-02-17
DE1728140B1 (en) 1972-05-04
US3588004A (en) 1971-06-28
GB1213505A (en) 1970-11-25

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Legal Events

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PL Patent ceased