JPS6467599A - Guided missile - Google Patents

Guided missile

Info

Publication number
JPS6467599A
JPS6467599A JP22562587A JP22562587A JPS6467599A JP S6467599 A JPS6467599 A JP S6467599A JP 22562587 A JP22562587 A JP 22562587A JP 22562587 A JP22562587 A JP 22562587A JP S6467599 A JPS6467599 A JP S6467599A
Authority
JP
Japan
Prior art keywords
compound
time
fins
stabilizer
specified
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.)
Pending
Application number
JP22562587A
Other languages
Japanese (ja)
Inventor
Ichiji Nishimura
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP22562587A priority Critical patent/JPS6467599A/en
Publication of JPS6467599A publication Critical patent/JPS6467599A/en
Pending legal-status Critical Current

Links

Landscapes

  • Circuit Breakers (AREA)

Abstract

PURPOSE: To enhance motion performance and aerodynamic stability while preventing mechanical interference with a mother machine by incorporating stabilizer fins in the body of a guided projectile and developing the fins by a torsional torque stored in a spiral spring with a specified time lag after launching through a locking unit-comprising a powder of time prolonging compound and output compound and a gas cylinder. CONSTITUTION: Torsional torque stored in a torsion bar 8 acts to develop stabilizer fins 3 through bevel gears 9, 10 and gears 12, 13 but it is blocked by a locking unit 7 and the fins 3 are retained in a contained state. When a body 1 is launched from an aircraft, an ignition plug 18 fires a time prolonging compound 19 based on an electric signal at the time of launching and the time proloning compound 19 fires an output compound 20 upon elapsing a specified combustion time. A piston 15 enters into ascending motion at that moment by the pressure of a large quantity of combustion gas generated from the output compound 20 and it is drawn out by a hole 16 made in the stabilizer fin 3. Since the quantity of the time prolonging compound 19 is selected, the fins are developed with a specified time lag after a projectile is launched from a mother machine.
JP22562587A 1987-09-09 1987-09-09 Guided missile Pending JPS6467599A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22562587A JPS6467599A (en) 1987-09-09 1987-09-09 Guided missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22562587A JPS6467599A (en) 1987-09-09 1987-09-09 Guided missile

Publications (1)

Publication Number Publication Date
JPS6467599A true JPS6467599A (en) 1989-03-14

Family

ID=16832241

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22562587A Pending JPS6467599A (en) 1987-09-09 1987-09-09 Guided missile

Country Status (1)

Country Link
JP (1) JPS6467599A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5734701A (en) * 1994-04-26 1998-03-31 Brother Kogyo Kabushiki Kaisha Information transmission/reception device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5734701A (en) * 1994-04-26 1998-03-31 Brother Kogyo Kabushiki Kaisha Information transmission/reception device
US6018569A (en) * 1994-04-26 2000-01-25 Brother Kogyo Kabushiki Kaisha Information transmission/reception device

Similar Documents

Publication Publication Date Title
YU45004B (en) Device for decreasing front resistance of projectiles
GB1143436A (en) Practice ammunition
US3750585A (en) Tracer projectiles
US2323303A (en) Incendiary bullet
GB1286723A (en) Improvements in shell cartridges
GB869410A (en) Improvements relating to projectiles and rockets
GB1465550A (en) Projectile launching device
JPS6467599A (en) Guided missile
FR2605399B1 (en) SHOTGUN GRENADE
JPS6467598A (en) Guided missile
ES8309002A1 (en) Gun cartridge for flat trajectory or high angle firing.
JPS6467600A (en) Guided missile
US2502442A (en) Colored smoke bomb
US3886841A (en) Rocket powered round
US1380172A (en) Self-propelled projectile
US2361955A (en) Explosive bullet
GB929601A (en) Improvements in projectiles fitted with an electric detonator operated by a generator of the inertia type
JPS6449899A (en) Guided missile
GB940479A (en) Improvements relating to rocket devices
SU323982A1 (en) METHOD FOR CRUSHING THE DIMENSIONS AND ELIMINATING THE DEPENDENCES OF THE MOUNTAIN MASS
JPS6463796A (en) Guided missile
JPS54100200A (en) Chaft bullet
GB1085177A (en) Improvements in rocket projectiles having a war-head
GB1248432A (en) Improvements in or relating to seismic charge assemblies for marine exploration purposes
GB904348A (en) Ammunition fuze