AT285381B - Rocket with folding tail and braking device - Google Patents

Rocket with folding tail and braking device

Info

Publication number
AT285381B
AT285381B AT848268A AT848268A AT285381B AT 285381 B AT285381 B AT 285381B AT 848268 A AT848268 A AT 848268A AT 848268 A AT848268 A AT 848268A AT 285381 B AT285381 B AT 285381B
Authority
AT
Austria
Prior art keywords
rocket
braking device
folding tail
tail
folding
Prior art date
Application number
AT848268A
Other languages
German (de)
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
Application granted granted Critical
Publication of AT285381B publication Critical patent/AT285381B/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)
  • Toys (AREA)
AT848268A 1967-09-06 1968-09-02 Rocket with folding tail and braking device AT285381B (en)

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
AT285381B true AT285381B (en) 1970-10-27

Family

ID=4383325

Family Applications (1)

Application Number Title Priority Date Filing Date
AT848268A AT285381B (en) 1967-09-06 1968-09-02 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)

Families Citing this family (19)

* 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
FR2716965B1 (en) * 1994-03-02 1996-05-03 Matra Defense Releasable machine with aerodynamic stabilization and braking.
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
NL236992A (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

Also Published As

Publication number Publication date
BE720311A (en) 1969-02-17
US3598345A (en) 1971-08-10
CH480612A (en) 1969-10-31
SE352728B (en) 1973-01-08
GB1209210A (en) 1970-10-21
DE1728103A1 (en) 1972-03-02
FR1603736A (en) 1971-05-24
NL6812718A (en) 1969-03-10
NL139209B (en) 1973-06-15

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