SE9800575L - pulse unit - Google Patents

pulse unit

Info

Publication number
SE9800575L
SE9800575L SE9800575A SE9800575A SE9800575L SE 9800575 L SE9800575 L SE 9800575L SE 9800575 A SE9800575 A SE 9800575A SE 9800575 A SE9800575 A SE 9800575A SE 9800575 L SE9800575 L SE 9800575L
Authority
SE
Sweden
Prior art keywords
projectile
impulse
caps
open
weights
Prior art date
Application number
SE9800575A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE520694C2 (en
SE9800575D0 (en
Inventor
Stig Johnsson
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Priority to SE9800575A priority Critical patent/SE520694C2/en
Publication of SE9800575D0 publication Critical patent/SE9800575D0/en
Publication of SE9800575L publication Critical patent/SE9800575L/en
Publication of SE520694C2 publication Critical patent/SE520694C2/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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The impulse device contains cylindrical-shaped impulse charge chambers (7) extending at right angles to the projectile length direction and open at the projectile periphery end. Impulse weights (8) are insertable into the chambers and have impulse caps which are closed at the projectile periphery end, but open at the opposite end. Propellent charges in the caps are connected to a detonator activated by command. The impulse weights can be fired out from the projectile upon command during flight in order to generate impulses used to correct projectile trajectory.
SE9800575A 1998-02-26 1998-02-26 Impulse device for in-flight correction of trajectory of shell or other projectile SE520694C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE9800575A SE520694C2 (en) 1998-02-26 1998-02-26 Impulse device for in-flight correction of trajectory of shell or other projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9800575A SE520694C2 (en) 1998-02-26 1998-02-26 Impulse device for in-flight correction of trajectory of shell or other projectile

Publications (3)

Publication Number Publication Date
SE9800575D0 SE9800575D0 (en) 1998-02-26
SE9800575L true SE9800575L (en) 1999-08-27
SE520694C2 SE520694C2 (en) 2003-08-12

Family

ID=20410305

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9800575A SE520694C2 (en) 1998-02-26 1998-02-26 Impulse device for in-flight correction of trajectory of shell or other projectile

Country Status (1)

Country Link
SE (1) SE520694C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPQ776300A0 (en) * 2000-05-25 2000-08-10 Metal Storm Limited Missile control

Also Published As

Publication number Publication date
SE520694C2 (en) 2003-08-12
SE9800575D0 (en) 1998-02-26

Similar Documents

Publication Publication Date Title
WO2006137949A3 (en) Kinetic energy rod warhead with lower deployment angles
DE69106913D1 (en) Torpedo warhead with hollow and explosive charge.
CA2527043A1 (en) Kinetic energy rod warhead with lower deployment angles
AU551191B2 (en) Non-electric blasting assembly
WO2000071965A3 (en) Non-lethal ballistic
DE3783094D1 (en) PROJECT-FORMING LOAD.
FR2435015A1 (en) PROJECTILE THAT CAN BE FIRED WITHOUT BACKUP AND WITHOUT DETONATION
DE69511906D1 (en) Firing device for a pyrotechnic charge with a detonator head, in particular for hand grenades, with three functions
DE69706738D1 (en) Projectile whose explosive charge is triggered by a target indicator
RU2002120899A (en) Anti-rocket and method of destruction of an approaching rocket
ES2194481T3 (en) REGULATION OF TIME INTERVALS IN A SEQUENCE OF EXPLOSIVE DETONATIONS.
SE9800575D0 (en) pulse unit
EP0339847A3 (en) A detonator
EP0318996A3 (en) Pyrotechnical initiator for projectiles, rockets, bomblets and mines
FR2701109B1 (en) Ignition device for projectiles, missiles, miniature bombs and mines with a pyrotechnic self-destruct device.
NO20015467L (en) Teeth for pyrotechnic delay charge
FR2534681B1 (en) IMPROVEMENTS IN PROJECTILE LAUNCHING WEAPON SYSTEMS, IN PARTICULAR FOR PROPELLANT LOADS AND INNER BALLISTICS
FI962545A0 (en) A method of repairing the trajectory of a cannon, grenade or rocket launcher or similar projectile
DE50012396D1 (en) Armor piercing ammo
EP0913663A3 (en) Pyrotechnic impact igniter
NO178945C (en) Detonator firing element, detonator with the firing element, and a blasting system involving several such detonators
SE9801826D0 (en) Robot Exercise Device
ES2077991T3 (en) PYROTECHNICAL GENERATOR OF IMPULSION FORCES WITHOUT SHOCK WAVE.
DK629286D0 (en) PACKAGE FOR PYROTECHNICAL CHARGING OR PROJECTILE
RU2002108265A (en) Detonating device

Legal Events

Date Code Title Description
NUG Patent has lapsed