CH479849A - Porietto autopropulso o semiautopropulso con governale ad alette retrattili - Google Patents

Porietto autopropulso o semiautopropulso con governale ad alette retrattili

Info

Publication number
CH479849A
CH479849A CH942568A CH942568A CH479849A CH 479849 A CH479849 A CH 479849A CH 942568 A CH942568 A CH 942568A CH 942568 A CH942568 A CH 942568A CH 479849 A CH479849 A CH 479849A
Authority
CH
Switzerland
Prior art keywords
propelled
self
porietto
governor
semi
Prior art date
Application number
CH942568A
Other languages
English (en)
Inventor
Pesarini Mario
Galeazzi Piero
Tosti Carlo
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 CH479849A publication Critical patent/CH479849A/it

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)
  • Support Of The Bearing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Rolling Contact Bearings (AREA)
CH942568A 1967-07-22 1968-06-24 Porietto autopropulso o semiautopropulso con governale ad alette retrattili CH479849A (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT3836067 1967-07-22

Publications (1)

Publication Number Publication Date
CH479849A true CH479849A (it) 1969-10-15

Family

ID=11246023

Family Applications (1)

Application Number Title Priority Date Filing Date
CH942568A CH479849A (it) 1967-07-22 1968-06-24 Porietto autopropulso o semiautopropulso con governale ad alette retrattili

Country Status (3)

Country Link
US (1) US3602459A (it)
CH (1) CH479849A (it)
DE (1) DE1703722C3 (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995031689A1 (en) * 1994-05-13 1995-11-23 Hughes Aircraft Company Missile with deployable control fins

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2041502B (en) * 1979-02-08 1982-09-08 British Aerospace Folding fin assembly
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
DE3515326A1 (de) * 1985-04-27 1986-10-30 Rheinmetall GmbH, 4000 Düsseldorf Nutzlastgeschoss
SE460436B (sv) * 1986-12-01 1989-10-09 Bofors Ab Anordning foer att minska rotationen och samtidigt aastadkomma en sidohastighet hos en roterande ammunitionsenhet
IL101730A (en) * 1992-04-30 1995-12-31 Israel State Moving body such as missile having wings erectable upon acceleration
US6168111B1 (en) * 1997-03-03 2001-01-02 The United States Of America As Represented By The Secretary Of The Army Fold-out fin
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
AU2017300113B2 (en) * 2016-07-21 2020-04-02 Chairman, Defence Research &Development Organisation (Drdo) Bi-directional wing unfolding mechanism
US11187505B1 (en) * 2019-07-03 2021-11-30 Gerhard W. Thielman Concatenated annular swing-wing tandem lift enhancer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995031689A1 (en) * 1994-05-13 1995-11-23 Hughes Aircraft Company Missile with deployable control fins

Also Published As

Publication number Publication date
DE1703722C3 (de) 1974-04-04
US3602459A (en) 1971-08-31
DE1703722A1 (de) 1972-04-27
DE1703722B2 (de) 1973-09-06

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Legal Events

Date Code Title Description
PL Patent ceased