BE608385A - Tailplane with retractable fins for projectiles with automatic or non-automatic propulsion, and projectile provided with this tail. - Google Patents

Tailplane with retractable fins for projectiles with automatic or non-automatic propulsion, and projectile provided with this tail.

Info

Publication number
BE608385A
BE608385A BE608385A BE608385A BE608385A BE 608385 A BE608385 A BE 608385A BE 608385 A BE608385 A BE 608385A BE 608385 A BE608385 A BE 608385A BE 608385 A BE608385 A BE 608385A
Authority
BE
Belgium
Prior art keywords
automatic
tailplane
projectiles
tail
propulsion
Prior art date
Application number
BE608385A
Other languages
French (fr)
Inventor
Francesco Moratti
Carlo Tosti
Original Assignee
Bombrini Parodi Delfino Spa
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 Bombrini Parodi Delfino Spa filed Critical Bombrini Parodi Delfino Spa
Publication of BE608385A publication Critical patent/BE608385A/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)
  • Toys (AREA)
  • Transmission Devices (AREA)
BE608385A 1960-10-12 1961-09-21 Tailplane with retractable fins for projectiles with automatic or non-automatic propulsion, and projectile provided with this tail. BE608385A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1757960 1960-10-12

Publications (1)

Publication Number Publication Date
BE608385A true BE608385A (en) 1962-01-15

Family

ID=11150442

Family Applications (1)

Application Number Title Priority Date Filing Date
BE608385A BE608385A (en) 1960-10-12 1961-09-21 Tailplane with retractable fins for projectiles with automatic or non-automatic propulsion, and projectile provided with this tail.

Country Status (5)

Country Link
US (1) US3127838A (en)
BE (1) BE608385A (en)
CH (1) CH385077A (en)
DE (1) DE1168804B (en)
GB (1) GB966035A (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
US3304030A (en) * 1965-09-24 1967-02-14 James E Weimholt Pyrotechnic-actuated folding fin assembly
SE340417B (en) * 1969-06-06 1971-11-15 Bofors Ab
NL7017521A (en) * 1969-12-03 1971-06-07
DE2841773C2 (en) * 1978-09-26 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Pivoting arrangement of the tail unit, especially in the case of missiles or projectiles
US4480806A (en) * 1982-11-08 1984-11-06 Stencel Aero Engineering Corporation Ejection seat stabilization apparatus
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
US4667899A (en) * 1984-11-28 1987-05-26 General Dynamics, Pomona Division Double swing wing self-erecting missile wing structure
DE3508103A1 (en) * 1985-03-07 1986-09-18 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Folding/collapsible wing
FR2623898B1 (en) * 1987-11-26 1990-03-23 France Etat Armement DEVICE FOR DEPLOYING A PROJECTILE FIN
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil
FR2655720A1 (en) * 1989-12-08 1991-06-14 Thomson Brandt Armements WING GALBEE DEPLOYABLE FOR FLYING ENGINE.
US6928400B2 (en) * 2001-10-02 2005-08-09 Raytheon Company Method for designing a deployment mechanism
CA2499956C (en) * 2002-11-18 2009-02-03 Raytheon Company Method for designing a fin deployment mechanism
US7642492B2 (en) * 2005-01-26 2010-01-05 Raytheon Company Single-axis fin deployment system
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
US10458764B2 (en) 2016-10-24 2019-10-29 Rosemount Aerospace Inc. Canard stowage lock
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
GB2587520B (en) * 2018-03-23 2022-09-21 Simmonds Precision Products Space saving wing stowage
CN110360897A (en) * 2019-06-28 2019-10-22 南京理工大学 A kind of stable Supercavitating Projectile enters water-bound
US11187505B1 (en) * 2019-07-03 2021-11-30 Gerhard W. Thielman Concatenated annular swing-wing tandem lift enhancer

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB189523823A (en) * 1895-12-12 1896-11-14 Martns Stevenson Calvert Improvements in Projectiles.
BE379532A (en) * 1930-05-22
US2700337A (en) * 1952-02-28 1955-01-25 James M Cumming Liquid propellent rocket
FR1187193A (en) * 1957-11-15 1959-09-08 Hotchkiss Brandt Deployable stabilizer for projectile
FR1191519A (en) * 1958-02-13 1959-10-20 Hotchkiss Brandt Deploying tail for artillery projectile
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin

Also Published As

Publication number Publication date
GB966035A (en) 1964-08-06
US3127838A (en) 1964-04-07
DE1168804B (en) 1964-04-23
CH385077A (en) 1965-02-26

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