CH321152A - Tail for projectile - Google Patents

Tail for projectile

Info

Publication number
CH321152A
CH321152A CH321152DA CH321152A CH 321152 A CH321152 A CH 321152A CH 321152D A CH321152D A CH 321152DA CH 321152 A CH321152 A CH 321152A
Authority
CH
Switzerland
Prior art keywords
projectile
tail
Prior art date
Application number
Other languages
French (fr)
Inventor
Jasse Joseph Raymond
Original Assignee
Brandt Soc Nouv Ets
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 Brandt Soc Nouv Ets filed Critical Brandt Soc Nouv Ets
Publication of CH321152A publication Critical patent/CH321152A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-around fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Emergency Lowering Means (AREA)
CH321152D 1953-12-21 1954-11-19 Tail for projectile CH321152A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1096579T 1953-12-21

Publications (1)

Publication Number Publication Date
CH321152A true CH321152A (en) 1957-04-30

Family

ID=9618185

Family Applications (1)

Application Number Title Priority Date Filing Date
CH321152D CH321152A (en) 1953-12-21 1954-11-19 Tail for projectile

Country Status (6)

Country Link
US (1) US2793591A (en)
BE (1) BE533456A (en)
CH (1) CH321152A (en)
FR (1) FR1096579A (en)
GB (1) GB753838A (en)
NL (2) NL236992A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1134316B (en) * 1958-04-04 1962-08-02 Bombrini Parodi Delfino Societ Rocket projectile with flap tail unit

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE551492A (en) * 1955-10-20 Brandt Soc Nouv Ets
US3295444A (en) * 1956-08-02 1967-01-03 Vincent J Cushing Dispersal type cluster warhead
US2858765A (en) * 1956-08-07 1958-11-04 Dale E Startzell Spring-loaded, locking hinge fin assembly
DE1083155B (en) * 1957-12-07 1960-06-09 Ilyana Von Thyssen Bornemisza Grenade launcher projectile
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
CH480612A (en) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rocket with folding tail and braking device
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
GB1523963A (en) * 1976-02-26 1978-09-06 Hawker Siddeley Dynamics Ltd Method and means for auxiliary control of vehicle direction
FR2356118A1 (en) * 1976-06-25 1978-01-20 Europ Propulsion EMPENNAGE FOR PROJECTILE
FR2655720A1 (en) * 1989-12-08 1991-06-14 Thomson Brandt Armements WING GALBEE DEPLOYABLE FOR FLYING ENGINE.
FR2786561B1 (en) * 1998-11-30 2001-12-07 Giat Ind Sa DEVICE FOR BRAKING IN TRANSLATION OF A PROJECTILE ON A TRAJECTORY
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
DE10205043C5 (en) * 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg From a tube to be closed missile with überkalibrigem tail
DE102006022248B3 (en) * 2006-05-12 2007-11-08 Lfk-Lenkflugkörpersysteme Gmbh Retaining device on wrapped wings of flying object, allowing reliable release of wings into working position, comprises controlled release holder on one wing and cooperating fixtures on others
US7628353B2 (en) * 2006-11-14 2009-12-08 Raytheon Company Delayed tail fin deployment mechanism and method
RU2375670C2 (en) * 2008-07-21 2009-12-10 Александр Михайлович Гультяев Rocket
KR101234218B1 (en) * 2010-06-25 2013-02-18 국방과학연구소 Wing device and flight vehicle having the same
US8640589B2 (en) 2010-07-20 2014-02-04 Raytheon Company Projectile modification method
US9593922B2 (en) * 2013-03-14 2017-03-14 Bae Systems Land & Armaments L.P. Fin deployment system
FR3071917B1 (en) * 2017-10-04 2021-11-19 Nexter Munitions WING AND PROJECTILE LOCKING DEVICE INCLUDING SUCH A DEVICE

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR494610A (en) * 1917-04-21 1919-09-13 Michel Cappella Finned and diamond-tipped shells
BE379532A (en) * 1930-05-22
GB514085A (en) * 1939-02-18 1939-10-30 Leslie Ernest Shilston Improvements in dart flights
US2421752A (en) * 1943-02-22 1947-06-10 Eureka Williams Corp Rocket projectile
US2465401A (en) * 1943-09-23 1949-03-29 Leslie A Skinner Rocket fin assembly
DE914933C (en) * 1953-04-23 1954-07-12 Oerlikon Buehrle Ag Rocket projectile with hinged stabilizing wings

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1134316B (en) * 1958-04-04 1962-08-02 Bombrini Parodi Delfino Societ Rocket projectile with flap tail unit

Also Published As

Publication number Publication date
FR1096579A (en) 1955-06-22
GB753838A (en) 1956-08-01
BE533456A (en)
US2793591A (en) 1957-05-28
NL236992A (en)
NL100549C (en)

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