CH480612A - Rocket with folding tail and braking device - Google Patents

Rocket with folding tail and braking device

Info

Publication number
CH480612A
CH480612A CH1247167A CH1247167A CH480612A CH 480612 A CH480612 A CH 480612A CH 1247167 A CH1247167 A CH 1247167A CH 1247167 A CH1247167 A CH 1247167A CH 480612 A CH480612 A CH 480612A
Authority
CH
Switzerland
Prior art keywords
rocket
braking device
folding tail
tail
folding
Prior art date
Application number
CH1247167A
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 CH1247167A priority Critical patent/CH480612A/en
Priority to SE10547/68A priority patent/SE352728B/xx
Priority to DE19681728103 priority patent/DE1728103C/en
Priority to FR1603736D priority patent/FR1603736A/fr
Priority to GB40794/68A priority patent/GB1209210A/en
Priority to BE720311D priority patent/BE720311A/xx
Priority to AT848268A priority patent/AT285381B/en
Priority to NL686812718A priority patent/NL139209B/en
Priority to US758067A priority patent/US3598345A/en
Publication of CH480612A publication Critical patent/CH480612A/en
Priority to NL727216150A priority patent/NL152079B/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)
  • Toys (AREA)
  • Braking Arrangements (AREA)
CH1247167A 1967-09-06 1967-09-06 Rocket with folding tail and braking device CH480612A (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
CH1247167A CH480612A (en) 1967-09-06 1967-09-06 Rocket with folding tail and braking device
SE10547/68A SE352728B (en) 1967-09-06 1968-08-05
DE19681728103 DE1728103C (en) 1967-09-06 1968-08-26 Folding tail with braking device for a rocket
FR1603736D FR1603736A (en) 1967-09-06 1968-08-26
GB40794/68A GB1209210A (en) 1967-09-06 1968-08-26 Rocket with folding fins and braking device
BE720311D BE720311A (en) 1967-09-06 1968-09-02
AT848268A AT285381B (en) 1967-09-06 1968-09-02 Rocket with folding tail and braking device
NL686812718A NL139209B (en) 1967-09-06 1968-09-06 MISSILE WITH A SPRAY PIPE BODY WHY A FOLDABLE GUIDE FACE ASSEMBLY IS FITTED
US758067A US3598345A (en) 1967-09-06 1968-09-06 Rocket with folding fins and braking device
NL727216150A NL152079B (en) 1967-09-06 1972-11-28 PROJECTILE WITH SWIVEL BRAKE FACES.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1247167A CH480612A (en) 1967-09-06 1967-09-06 Rocket with folding tail and braking device

Publications (1)

Publication Number Publication Date
CH480612A true CH480612A (en) 1969-10-31

Family

ID=4383325

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1247167A CH480612A (en) 1967-09-06 1967-09-06 Rocket with folding tail and braking device

Country Status (8)

Country Link
US (1) US3598345A (en)
AT (1) AT285381B (en)
BE (1) BE720311A (en)
CH (1) CH480612A (en)
FR (1) FR1603736A (en)
GB (1) GB1209210A (en)
NL (1) NL139209B (en)
SE (1) SE352728B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2716965A1 (en) * 1994-03-02 1995-09-08 Matra Defense Releasable machine with aerodynamic stabilization and braking.

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2227104C2 (en) * 1972-06-03 1982-07-15 Dynamit Nobel Ag, 5210 Troisdorf Projectile or missile with a hinged tail unit
US3978790A (en) * 1975-10-23 1976-09-07 The Boeing Company High altitude sonobuoy
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
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
SE445952B (en) * 1983-03-25 1986-07-28 Bofors Ab DEVICE FOR REDUCING PROJECT DISTRIBUTION
DE3507677A1 (en) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg MISSILE WITH OVER-CALIBRATE ANALYSIS
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
DE19827278A1 (en) * 1998-06-19 1999-12-23 Diehl Stiftung & Co Steerable missile can be launched by thrust of propellant gas charge
GB9813558D0 (en) * 1998-06-24 2002-03-06 Royal Ordnance Plc Device for exerting drag
US6079342A (en) * 1999-02-03 2000-06-27 Tseng; Hsien Chang Needle support for sewing machine
RU2166179C1 (en) * 2000-06-26 2001-04-27 Государственное унитарное предприятие Брянский химический завод Jet projectile
RU2176068C1 (en) * 2000-07-28 2001-11-20 Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" Jet projectile launched from launching tube
US6695252B1 (en) * 2002-09-18 2004-02-24 Raytheon Company Deployable fin projectile with outflow device
FR2895071B1 (en) * 2005-12-19 2008-01-18 Giat Ind Sa ANTI-REBOUND LOCKING DEVICE OF A DEPLOYABLE FIN OF A PROJECTILE.
US9702670B2 (en) * 2012-08-21 2017-07-11 Omnitek Partners Llc Countermeasure flares
CN105674813B (en) * 2014-11-19 2017-11-21 中国科学院沈阳自动化研究所 A kind of hot blade hook lock separating mechanism
RU2642693C2 (en) * 2016-04-21 2018-01-25 Акционерное общество "Новосибирский завод искусственного волокна" Supersonic projectile
CN113237393A (en) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 High-precision stabilizing device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE533456A (en) * 1953-12-21 Brandt Soc Nouv Ets
US2942545A (en) * 1954-11-23 1960-06-28 Gordon L Fogal Stabilizing system for mine dropped from aircraft
US2941764A (en) * 1957-08-08 1960-06-21 Electronics Corp America Flaps for supersonic aircraft escape systems
CH385678A (en) * 1961-07-19 1964-12-15 Oerlikon Buehrle Ag Rocket projectile with spreading tail
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2716965A1 (en) * 1994-03-02 1995-09-08 Matra Defense Releasable machine with aerodynamic stabilization and braking.
EP0675334A1 (en) * 1994-03-02 1995-10-04 Matra Defense Aerodynamic stabilisation and braking device for air-drop body

Also Published As

Publication number Publication date
BE720311A (en) 1969-02-17
US3598345A (en) 1971-08-10
NL139209B (en) 1973-06-15
GB1209210A (en) 1970-10-21
FR1603736A (en) 1971-05-24
SE352728B (en) 1973-01-08
DE1728103A1 (en) 1972-03-02
NL6812718A (en) 1969-03-10
AT285381B (en) 1970-10-27

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Legal Events

Date Code Title Description
PL Patent ceased