PROBLEM TO BE SOLVED: To provide a technology for improving accuracy when a missile propulsion direction is controlled toward a prescribed direction.SOLUTION: This invention relates to a missile propulsion direction control device 100 for changing an orientation of a gas injection nozzle main body 101 for missile propulsion to control a propulsion direction of the missile comprising a nozzle main body holding part 102 for holding the gas injection nozzle main body 101; a first actuator 110 for connecting the nozzle main body holding part 102 and the gas injection nozzle main body 101 to each other and changing an angle of the gas injection nozzle main body 101 with respect to the missile; and a second actuator 120 installed at a connected part between the missile and the nozzle main body holding part 102 so as to turn a gas injection nozzle module capable of changing an angle of the gas injection nozzle main body 101 by the first actuator 110 with respect to the missile.SELECTED DRAWING: Figure 1

    【課題】 飛翔体の推進方向を所定の向きに制御する際の精度を向上する技術を提供する。【解決手段】 飛翔体推進用のガス噴射ノズル本体101の向きを変更して飛翔体の推進方向を制御する飛翔体推進方向制御装置100であって、前記ガス噴射ノズル本体101を保持するノズル本体保持部102と、前記ノズル本体保持部102及び前記ガス噴射ノズル本体101を相互に連結し、前記飛翔体に対する前記ガス噴射ノズル本体101の角度を変更する第1アクチュエータ110と、前記飛翔体及び前記ノズル本体保持部102の連結部に設けられ、前記第1アクチュエータ120によって前記ガス噴射ノズル本体101の角度を変更可能なガス噴射ノズルモジュールを前記飛翔体に対して回動させる第2アクチュエータ120とを備えたことを特徴とする。【選択図】図1


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    Title :

    MISSILE PROPULSION DIRECTION CONTROL DEVICE AND MISSILE


    Additional title:

    飛翔体推進方向制御装置及び飛翔体


    Contributors:

    Publication date :

    2016-04-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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