JPH0482599U - - Google Patents

Info

Publication number
JPH0482599U
JPH0482599U JP11877390U JP11877390U JPH0482599U JP H0482599 U JPH0482599 U JP H0482599U JP 11877390 U JP11877390 U JP 11877390U JP 11877390 U JP11877390 U JP 11877390U JP H0482599 U JPH0482599 U JP H0482599U
Authority
JP
Japan
Prior art keywords
volatile liquid
utility
model registration
tip
releasing
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
JP11877390U
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 JP11877390U priority Critical patent/JPH0482599U/ja
Publication of JPH0482599U publication Critical patent/JPH0482599U/ja
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/34Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
    • 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/40Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
    • 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/42Streamlined projectiles
    • F42B10/46Streamlined nose cones; Windshields; Radomes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Details Of Aerials (AREA)

Description

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

第1図はこの考案の一実施例を示す説明図、第
2図から第7図はこの考案の他の実施例を示す説
明図、第8図は従来の誘導飛しよう体の説明図で
ある。 図において、1は光学センサ、2は光学ドーム
、3は衝撃波、4は揮発性液体容器、5はポンプ
、6は配管、7は放出孔、8は気密容器である。
なお、図中同一符号は同一または相当部分をしめ
す。
Fig. 1 is an explanatory diagram showing one embodiment of this invention, Figs. 2 to 7 are explanatory diagrams showing other embodiments of this invention, and Fig. 8 is an explanatory diagram of a conventional guided flying object. . In the figure, 1 is an optical sensor, 2 is an optical dome, 3 is a shock wave, 4 is a volatile liquid container, 5 is a pump, 6 is piping, 7 is a discharge hole, and 8 is an airtight container.
Note that the same reference numerals in the figures indicate the same or equivalent parts.

Claims (1)

【実用新案登録請求の範囲】 (1) 光学センサにより目標を捕捉する誘導制御
装置を有する誘導飛しよう体において、光学ドー
ムと揮発性液体容器とポンプと上記誘導制御装置
内に設けられた配管と上記光学ドームの先端中心
軸上に設けられ上記配管の先端に接続された揮発
性液体放出用の穴とを備えたことを特徴とする誘
導飛しよう体。 (2) 複数の配管と光学ドーム上に設けられ上記
配管の先端に接続された複数の揮発性液体放出用
の穴とを備えた実用新案登録請求の範囲第(1)項
記載の誘導飛しよう体。 (3) 誘導制御装置外に設けられ先端が光学ドー
ムの先端中心軸上に位置し先端に揮発性液体放出
用の穴を有する配管を備えた実用新案登録請求の
範囲第(1)項記載の誘導飛しよう体。 (4) 誘導制御装置外に設けられ先端が光学ドー
ム上に位置し先端に揮発性液体放出用の穴を有す
る複数の配管を備えた実用新案登録請求の範囲第
(1)項記載の誘導飛しよう体。 (5) 誘導制御装置外に設けられ光学ドーム上に
位置し複数の揮発性液体放出用の穴を有する配管
を備えた実用新案登録請求の範囲第(1)項記載の
誘導飛しよう体。 (6) 光学センサを封入する気密容器と光学ドー
ムの先端中心軸上に設けられた揮発性液体放出用
の穴とを備えた実用新案登録請求の範囲第(1)項
記載の誘導飛しよう体。 (7) 光学センサを封入する気密容器と光学ドー
ム上に設けられた複数の揮発性液体放出用の穴と
を備えた実用新案登録請求の範囲第(1)項記載の
誘導飛しよう体。
[Scope of Claim for Utility Model Registration] (1) In a guided flying object having a guidance control device that captures a target using an optical sensor, an optical dome, a volatile liquid container, a pump, and piping provided in the guidance control device; A guided flying object characterized by comprising a volatile liquid discharge hole provided on the central axis of the tip of the optical dome and connected to the tip of the piping. (2) A guided flying vehicle according to claim (1) of the utility model registration claim, which is provided with a plurality of pipes and a plurality of holes for releasing a volatile liquid provided on the optical dome and connected to the tips of the pipes. body. (3) Utility model registration claim 1, which is provided with a pipe provided outside the guidance control device, the tip of which is located on the central axis of the tip of the optical dome, and which has a hole for releasing volatile liquid at the tip. Guided flying body. (4) Scope of Utility Model Registration Claim No. 1, which is provided outside the guidance control device and includes a plurality of pipes whose tips are located above the optical dome and whose tips have holes for releasing volatile liquid.
Guided projectiles as described in (1). (5) The guided flying object according to claim (1) of the utility model registration, which is provided with a pipe provided outside the guidance control device, located on the optical dome, and having a plurality of holes for releasing a volatile liquid. (6) A guided flying object as set forth in claim (1) of the utility model registration claim, which is equipped with an airtight container enclosing an optical sensor and a hole for releasing a volatile liquid provided on the central axis of the tip of an optical dome. . (7) A guided flying object according to claim (1) of the utility model registration, comprising an airtight container enclosing an optical sensor and a plurality of holes for releasing a volatile liquid provided on the optical dome.
JP11877390U 1990-11-13 1990-11-13 Pending JPH0482599U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11877390U JPH0482599U (en) 1990-11-13 1990-11-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11877390U JPH0482599U (en) 1990-11-13 1990-11-13

Publications (1)

Publication Number Publication Date
JPH0482599U true JPH0482599U (en) 1992-07-17

Family

ID=31866734

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11877390U Pending JPH0482599U (en) 1990-11-13 1990-11-13

Country Status (1)

Country Link
JP (1) JPH0482599U (en)

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