FR1134930A - Deployable stabilizer for projectile - Google Patents

Deployable stabilizer for projectile

Info

Publication number
FR1134930A
FR1134930A FR1134930DA FR1134930A FR 1134930 A FR1134930 A FR 1134930A FR 1134930D A FR1134930D A FR 1134930DA FR 1134930 A FR1134930 A FR 1134930A
Authority
FR
France
Prior art keywords
projectile
deployable
stabilizer
deployable stabilizer
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BRANDT SOC NOUV ETS
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
Application granted granted Critical
Publication of FR1134930A publication Critical patent/FR1134930A/en
Expired legal-status Critical Current

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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
FR1134930D 1955-10-20 1955-10-20 Deployable stabilizer for projectile Expired FR1134930A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1038951X 1955-10-20

Publications (1)

Publication Number Publication Date
FR1134930A true FR1134930A (en) 1957-04-19

Family

ID=9587986

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1134930D Expired FR1134930A (en) 1955-10-20 1955-10-20 Deployable stabilizer for projectile

Country Status (7)

Country Link
US (1) US2924175A (en)
BE (1) BE551492A (en)
CH (1) CH333219A (en)
DE (1) DE1038951B (en)
FR (1) FR1134930A (en)
GB (1) GB795045A (en)
NL (2) NL104379C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2559256A1 (en) * 1984-02-02 1985-08-09 Dynamit Nobel Ag MISSILE PROVIDED WITH A STYLING PLACED AT THE REAR END OF ITS FUSELAGE

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL250199A (en) * 1959-04-13
US3103886A (en) * 1960-10-13 1963-09-17 Charles H Popenoe Coiling fin for tube launched missiles
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
US3273500A (en) * 1965-01-25 1966-09-20 Kongelbeck Sverre Self-erecting folding fin
US3695556A (en) * 1970-08-03 1972-10-03 Us Navy Hinged stability and control fin assembly
US3952970A (en) * 1974-08-28 1976-04-27 The United States Of America As Represented By The Secretary Of The Navy Means for improving rocket missile accuracy
DE2637461C2 (en) * 1976-08-20 1982-07-15 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Tail unit for a missile
AU524255B2 (en) * 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
US4336914A (en) * 1978-12-29 1982-06-29 The Commonwealth Of Australia Deployable wing mechanism
SE464833B (en) * 1989-10-20 1991-06-17 Bofors Ab SUBSCRIPTION PART WITH SWINGABLY ORGANIZED MEAL DETECTOR AND BARE AREA
US5085381A (en) * 1991-03-29 1992-02-04 The United States Of America As Represented By The Secretary Of The Air Force Deployable aerodynamic aerosurface
US6092264A (en) * 1998-11-13 2000-07-25 Lockheed Martin Corporation Single axis fold actuator and lock for member
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
FR2910122B1 (en) * 2006-12-15 2009-03-06 Thales Sa DEPLOYABLE CARRIER EMPLOYING DEVICE FOR OBUS
KR101234218B1 (en) * 2010-06-25 2013-02-18 국방과학연구소 Wing device and flight vehicle having the same
US9593922B2 (en) * 2013-03-14 2017-03-14 Bae Systems Land & Armaments L.P. Fin deployment system
CN105620722A (en) * 2014-10-29 2016-06-01 北京临近空间飞行器系统工程研究所 Folding wing rudder miniaturized unfolding structure based on thermosensitive shape memory alloy
DE102015014368A1 (en) 2015-11-06 2017-05-11 Mbda Deutschland Gmbh Folding wing for a missile and a missile with at least one folding wing arranged thereon
US10752334B2 (en) * 2016-09-30 2020-08-25 Edward Chow Collapsible and rapidly-deployable unmanned aerial vehicle
DE102017113058B4 (en) 2017-06-14 2023-04-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. space transport aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1448166A (en) * 1918-05-15 1923-03-13 Edw Fay Wilson Projectile
FR1061242A (en) * 1952-08-05 1954-04-09 Development of rocket projectiles with deployable tail fins
BE527578A (en) * 1953-04-23
NL236992A (en) * 1953-12-21 Brandt Soc Nouv Ets
FR1104534A (en) * 1954-05-13 1955-11-21 Soc Tech De Rech Ind Deployable tail

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2559256A1 (en) * 1984-02-02 1985-08-09 Dynamit Nobel Ag MISSILE PROVIDED WITH A STYLING PLACED AT THE REAR END OF ITS FUSELAGE

Also Published As

Publication number Publication date
DE1038951B (en) 1958-09-11
BE551492A (en)
NL211396A (en)
NL104379C (en)
US2924175A (en) 1960-02-09
CH333219A (en) 1958-10-15
GB795045A (en) 1958-05-14

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