FR1511835A - Mechanism for the deployment of fins hingedly connected to a jet propelled missile - Google Patents

Mechanism for the deployment of fins hingedly connected to a jet propelled missile

Info

Publication number
FR1511835A
FR1511835A FR95266A FR95266A FR1511835A FR 1511835 A FR1511835 A FR 1511835A FR 95266 A FR95266 A FR 95266A FR 95266 A FR95266 A FR 95266A FR 1511835 A FR1511835 A FR 1511835A
Authority
FR
France
Prior art keywords
deployment
hingedly connected
jet propelled
propelled missile
fins
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
FR95266A
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.)
Bolkow GmbH
Original Assignee
Bolkow GmbH
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 Bolkow GmbH filed Critical Bolkow GmbH
Application granted granted Critical
Publication of FR1511835A publication Critical patent/FR1511835A/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
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR95266A 1966-02-24 1967-02-16 Mechanism for the deployment of fins hingedly connected to a jet propelled missile Expired FR1511835A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB0085933 1966-02-24

Publications (1)

Publication Number Publication Date
FR1511835A true FR1511835A (en) 1968-02-02

Family

ID=6983138

Family Applications (1)

Application Number Title Priority Date Filing Date
FR95266A Expired FR1511835A (en) 1966-02-24 1967-02-16 Mechanism for the deployment of fins hingedly connected to a jet propelled missile

Country Status (2)

Country Link
FR (1) FR1511835A (en)
GB (1) GB1174120A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4119613C2 (en) * 1991-06-14 1997-03-27 Diehl Gmbh & Co Missiles with fold-out guidance devices
DE10015514B4 (en) 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Wing stabilized projectile

Also Published As

Publication number Publication date
GB1174120A (en) 1969-12-10

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