To provide an augmented aerospike nozzle, an engine including an augmented aerospike nozzle, and a vehicle including an engine.SOLUTION: An augmented aerospike nozzle includes a throat, a center body extending rearward of the throat, an inside expansion surface defined by the center body, an outside expansion surface outward of the inside expansion surface, and an expansion cavity defined between the inside expansion surface and the outside expansion surface. The engine includes a high pressure chamber and the augmented aerospike nozzle. A vehicle for supersonic flight includes an engine having the augmented aerospike nozzle.SELECTED DRAWING: Figure 5

    【課題】増強型エアロスパイクノズル、増強型エアロスパイクノズルを含むエンジン、及びエンジンを含むビークルに関する。【解決手段】増強型エアロスパイクノズルは、スロートと、スロートの後方に伸びるセンターボディと、センターボディによって規定される内側膨張面と、内側膨張面の外側の外側膨張面と、内側膨張面と外側膨張面の間に規定される膨張キャビティと、を含む。エンジンは高圧室と増強型エアロスパイクノズルとを含む。超音速飛行用のビークルは、増強型エアロスパイクノズルを有するエンジンを含む。【選択図】図5


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    Title :

    MULTISTAGE ROCKET, AND ATMOSPHERIC RE-ENTRY VEHICLE


    Additional title:

    多段式ロケット、大気圏再突入ビークル


    Contributors:

    Publication date :

    2024-09-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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