[go: up one dir, main page]

FR1061242A - Development of rocket projectiles with deployable tail fins - Google Patents

Development of rocket projectiles with deployable tail fins

Info

Publication number
FR1061242A
FR1061242A FR1061242DA FR1061242A FR 1061242 A FR1061242 A FR 1061242A FR 1061242D A FR1061242D A FR 1061242DA FR 1061242 A FR1061242 A FR 1061242A
Authority
FR
France
Prior art keywords
development
tail fins
rocket projectiles
deployable tail
deployable
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)
Inventor
Roger-Aime Robert
Pierre Matge
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 filed Critical
Application granted granted Critical
Publication of FR1061242A publication Critical patent/FR1061242A/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)
FR1061242D 1952-08-05 1952-08-05 Development of rocket projectiles with deployable tail fins Expired FR1061242A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1061242T 1952-08-05

Publications (1)

Publication Number Publication Date
FR1061242A true FR1061242A (en) 1954-04-09

Family

ID=9600069

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1061242D Expired FR1061242A (en) 1952-08-05 1952-08-05 Development of rocket projectiles with deployable tail fins

Country Status (1)

Country Link
FR (1) FR1061242A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1038951B (en) * 1955-10-20 1958-09-11 Brandt Soc Nouv Ets Folding wing tail unit for rockets or other projectiles
DE1041393B (en) * 1956-08-11 1958-10-16 Boelkow Entwicklungen Kg Flying body with rigid wings extending transversely to its longitudinal axis in different planes
DE1123597B (en) * 1958-02-13 1962-02-08 Hotchkiss Brandt Foldable stabilizing fins for an artillery shell to be fired from a gun barrel
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
EP0242180A3 (en) * 1986-04-15 1989-04-26 British Aerospace Public Limited Company Deployment arrangement for spinning body

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1038951B (en) * 1955-10-20 1958-09-11 Brandt Soc Nouv Ets Folding wing tail unit for rockets or other projectiles
DE1041393B (en) * 1956-08-11 1958-10-16 Boelkow Entwicklungen Kg Flying body with rigid wings extending transversely to its longitudinal axis in different planes
DE1123597B (en) * 1958-02-13 1962-02-08 Hotchkiss Brandt Foldable stabilizing fins for an artillery shell to be fired from a gun barrel
US3031967A (en) * 1958-02-13 1962-05-01 Hotchkiss Brandt Fin arrangement for projectiles
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
EP0242180A3 (en) * 1986-04-15 1989-04-26 British Aerospace Public Limited Company Deployment arrangement for spinning body

Similar Documents

Publication Publication Date Title
CH333219A (en) Deployable winged tail for projectile
FR1077914A (en) Ultra-sensitive head projectile
FR1077997A (en) Projectiles
FR1097883A (en) Rocket projectile with retractable tail
CH348629A (en) Deployable tail for artillery projectile
FR1070547A (en) Ignition fuse for rocket projectiles
FR1066178A (en) Improvements made to shaped explosive projectiles
FR1072919A (en) Exercise projectile
FR1061242A (en) Development of rocket projectiles with deployable tail fins
FR1079189A (en) Rocket with removable fins
CH332850A (en) Self-propelled projectile with retractable tail
FR1165002A (en) Shaped charge projectile
CH317932A (en) Percussion rocket
FR1149810A (en) Explosive charge projectile
FR62851E (en) Shaped charge projectile for rifled tubes
FR1076264A (en) Improvements to explosive armor-piercing projectiles
FR68861E (en) Projectile rocket improvements
FR1207513A (en) rocket and missile folding fin equipment
CH316794A (en) Anti-tank aviation grenade
FR1063268A (en) Rocket
FR1036037A (en) Cartridges and shaped charge projectiles
FR1105059A (en) Aircraft construction
FR1057447A (en) Projectile rocket improvements
CH324708A (en) High explosive incendiary grenade
FR1055325A (en) Improvements to shaped charge explosive projectiles