JPS6438498U - - Google Patents

Info

Publication number
JPS6438498U
JPS6438498U JP13394287U JP13394287U JPS6438498U JP S6438498 U JPS6438498 U JP S6438498U JP 13394287 U JP13394287 U JP 13394287U JP 13394287 U JP13394287 U JP 13394287U JP S6438498 U JPS6438498 U JP S6438498U
Authority
JP
Japan
Prior art keywords
propulsion device
hypersonic
subsonic
guided missile
penetrator
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
JP13394287U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP13394287U priority Critical patent/JPS6438498U/ja
Publication of JPS6438498U publication Critical patent/JPS6438498U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第１図は本考案の一実施例に係る誘導弾を示す
断面図、第２図は第１図に示す誘導弾の飛翔状態
を示す説明図、第３図は従来の誘導弾を示す断面
図、第４図は従来の誘導弾の飛翔状態を示す説明
図である。 １……誘導弾本体、２……ペネトレータ、４…
…小型ロケツト推進器、２０……亜音速用推進手
段、２１……極超音速用推進手段。 FIG. 1 is a sectional view showing a guided missile according to an embodiment of the present invention, FIG. 2 is an explanatory diagram showing the flight state of the guided missile shown in FIG. 1, and FIG. 3 is a sectional view showing a conventional guided missile. , FIG. 4 is an explanatory diagram showing the flight state of a conventional guided missile. 1... Guided missile body, 2... Penetrator, 4...
...Small rocket propulsion device, 20... Subsonic propulsion means, 21... Hypersonic propulsion means.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 亜音速で飛翔させる亜音速用推進手段と、短時
間で極超音速域まで加速させる極超音速用推進手
段と、運動エネルギーにより装甲を貫通するペネ
トレータとを有する誘導弾。 A guided missile that has a subsonic propulsion device that allows it to fly at subsonic speeds, a hypersonic propulsion device that accelerates it to the hypersonic range in a short time, and a penetrator that uses kinetic energy to penetrate armor.
JP13394287U 1987-09-03 1987-09-03 Pending JPS6438498U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13394287U JPS6438498U (en) 1987-09-03 1987-09-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13394287U JPS6438498U (en) 1987-09-03 1987-09-03

Publications (1)

Publication Number Publication Date
JPS6438498U true JPS6438498U (en) 1989-03-08

Family

ID=31392268

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13394287U Pending JPS6438498U (en) 1987-09-03 1987-09-03

Country Status (1)

Country Link
JP (1) JPS6438498U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07294196A (en) * 1994-04-27 1995-11-10 Nec Corp Guide controller for missile

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07294196A (en) * 1994-04-27 1995-11-10 Nec Corp Guide controller for missile

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