FR2390704A1 - Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target - Google Patents

Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

Info

Publication number
FR2390704A1
FR2390704A1 FR7714767A FR7714767A FR2390704A1 FR 2390704 A1 FR2390704 A1 FR 2390704A1 FR 7714767 A FR7714767 A FR 7714767A FR 7714767 A FR7714767 A FR 7714767A FR 2390704 A1 FR2390704 A1 FR 2390704A1
Authority
FR
France
Prior art keywords
charge
propelling
launching
separates
self
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.)
Granted
Application number
FR7714767A
Other languages
French (fr)
Other versions
FR2390704B1 (en
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.)
Ruggieri SA
Original Assignee
Ruggieri SA
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 Ruggieri SA filed Critical Ruggieri SA
Priority to FR7714767A priority Critical patent/FR2390704A1/en
Publication of FR2390704A1 publication Critical patent/FR2390704A1/en
Application granted granted Critical
Publication of FR2390704B1 publication Critical patent/FR2390704B1/fr
Granted 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding

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)

Abstract

The rear end of the firework or missile assembly has a tapered secton (2) and fins (3) to give stable flight direction and the projective carries a charge appropriate to its use. At a determined point in its flight this can be fired and separation can take place. The missile carries a propulsive charge (13) and a methode of ensuring that the separated part and its charge, very quickly can fall in a vertical direction. The propulsive charge can be powder or gas. If of powder it is in the form of a block or variable section or it can be of several powders of different combustion speeds. The pyrotechnic charge is held in a case (12).
FR7714767A 1977-05-13 1977-05-13 Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target Granted FR2390704A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7714767A FR2390704A1 (en) 1977-05-13 1977-05-13 Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7714767A FR2390704A1 (en) 1977-05-13 1977-05-13 Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

Publications (2)

Publication Number Publication Date
FR2390704A1 true FR2390704A1 (en) 1978-12-08
FR2390704B1 FR2390704B1 (en) 1980-02-29

Family

ID=9190797

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7714767A Granted FR2390704A1 (en) 1977-05-13 1977-05-13 Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target

Country Status (1)

Country Link
FR (1) FR2390704A1 (en)

Also Published As

Publication number Publication date
FR2390704B1 (en) 1980-02-29

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Legal Events

Date Code Title Description
ST Notification of lapse