To provide a circulation engine for artificial satellite propulsion.SOLUTION: A propulsion material high-pressure injection engine 1 is heated by heat or electricity sent from a small nuclear engine 10 via a pipe 8, and the propulsion material 12 is injected from an injection hole 13 by making it into a high pressure gas. The propulsion material 12 is rapidly cooled (about -180 degrees) by a propulsion energy dissolving device tank 2 to become liquid, is recovered with circulation gas 11 by a propulsion material recovery device 6, and is sent through a pipe 4 to a propulsion material tank 8 by a propulsion material pump 7 to be recovered. The propulsion material 12 recovered in this repetition is injected with a propulsion material feed pump 9 by the propulsion material high-pressure injection engine 1, and the propulsion power is transmitted to a rocket. The propulsion material 12 is converted into liquid by the propulsion energy dissolving device tank 2, and the energy is converted into heat and recovered.SELECTED DRAWING: Figure 1

    【課題】人工衛星推進用の循環エンジンを提供する。【解決手段】小型原子力エンジン10からパイプ8で送られた熱又は電気で推進材高圧噴射エンジン1を温め、推進材12を気体の高圧力にし噴射孔13より噴射する。推進剤12は推進エネルギー解消装置タンク2で急速(-180度前後)に冷やされ液体になり循環ガス11で推進材回収装置6により回収され、パイプ4を通り推進材ポンプ7で推進材タンク8に送られ回収される。この繰り返しで回収された推進材12は、推進材送りポンプ9で推進材高圧噴射エンジン1により噴射し、推進力はロケットに伝えられる。推進エネルギー解消装置タンク2により推進材12は液体になり、エネルギーは熱に変換され回収される。【選択図】図1


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    Titel :

    ARTIFICIAL SATELLITE PROPULSION MATERIAL CIRCULATION ENGINE


    Weitere Titelangaben:

    人工衛星推進材循環エンジン


    Beteiligte:
    TSUNODA YUKIO (Autor:in)

    Erscheinungsdatum :

    07.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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