FR2008535A1 - Stabilised missile propulsion system - Google Patents

Stabilised missile propulsion system

Info

Publication number
FR2008535A1
FR2008535A1 FR6913406A FR6913406A FR2008535A1 FR 2008535 A1 FR2008535 A1 FR 2008535A1 FR 6913406 A FR6913406 A FR 6913406A FR 6913406 A FR6913406 A FR 6913406A FR 2008535 A1 FR2008535 A1 FR 2008535A1
Authority
FR
France
Prior art keywords
projectile
barrel
casing
stabilised
under
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.)
Withdrawn
Application number
FR6913406A
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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
Priority claimed from DE19681703407 external-priority patent/DE1703407A1/en
Priority claimed from DE19686803618 external-priority patent/DE6803618U/en
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of FR2008535A1 publication Critical patent/FR2008535A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/10Cartridges, i.e. cases with charge and missile with self-propelled bullet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Photoreceptors In Electrophotography (AREA)

Abstract

Propulsion surface is discoid and located between propulsive charge and an under-bore projectile pref. seated on the tail of stabilising (1) device. Thus the projectile is supported and centered in an unrifled barrel by longitudinal ribs, formed of the (1) wings which are folded in a star towards front of projectile casing and tilt radially of the barrel outlet. Advantages are (a) firing a stabilised, under-bore projectile from an unrifled barrel under high shock; (b) minimal overall length in consideration of transporting weapon; very easy loading. More specifically the ribs are disposed about a cylinder of separate sections; latter is dividing into units after beginning of shot. The casing preferably retracts and has an annular throat fitted with airtight bush similar to a piston ring, having a wall cut away to the rear and projecting from the outside casing of the propulsion surface.
FR6913406A 1968-05-15 1969-04-28 Stabilised missile propulsion system Withdrawn FR2008535A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19681703407 DE1703407A1 (en) 1968-05-15 1968-05-15 Tail stabilized sabot bullet
DE19686803618 DE6803618U (en) 1968-10-24 1968-10-24 LIDING FOR BULLETS

Publications (1)

Publication Number Publication Date
FR2008535A1 true FR2008535A1 (en) 1970-01-23

Family

ID=25754666

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6913406A Withdrawn FR2008535A1 (en) 1968-05-15 1969-04-28 Stabilised missile propulsion system

Country Status (4)

Country Link
BE (1) BE732897A (en)
CH (1) CH510246A (en)
FR (1) FR2008535A1 (en)
SE (1) SE356361B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0677717A1 (en) * 1994-04-13 1995-10-18 DIEHL GMBH & CO. Projectile remotely controlled by means of a laser guiding beam
FR2768809A1 (en) * 1997-09-24 1999-03-26 Giat Ind Sa LARGE CALIBER LONG RANGE FIELD ARTILLERY PROJECTILE
WO2011137958A1 (en) * 2010-05-04 2011-11-10 Rheinmetall Waffe Munition Gmbh Projectile having a wing guide mechanism
WO2022038044A1 (en) 2020-08-17 2022-02-24 Isorg System for acquiring high-resolution images

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE8406351L (en) * 1984-12-13 1986-04-21 Ffv Affersverket GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0677717A1 (en) * 1994-04-13 1995-10-18 DIEHL GMBH & CO. Projectile remotely controlled by means of a laser guiding beam
FR2768809A1 (en) * 1997-09-24 1999-03-26 Giat Ind Sa LARGE CALIBER LONG RANGE FIELD ARTILLERY PROJECTILE
EP0905473A1 (en) * 1997-09-24 1999-03-31 Giat Industries Large-calibre long range projectile for artillery
US6234082B1 (en) 1997-09-24 2001-05-22 Giat Industries Large-caliber long-range field artillery projectile
WO2011137958A1 (en) * 2010-05-04 2011-11-10 Rheinmetall Waffe Munition Gmbh Projectile having a wing guide mechanism
WO2022038044A1 (en) 2020-08-17 2022-02-24 Isorg System for acquiring high-resolution images

Also Published As

Publication number Publication date
SE356361B (en) 1973-05-21
CH510246A (en) 1971-07-15
BE732897A (en) 1969-10-16

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Legal Events

Date Code Title Description
ST Notification of lapse