Provided is a detent apparatus for a rocket, The detent apparatus includes a detent including a first end portion, a second end portion opposite to the first end portion, an extension extending between the first end portion and the second end portion, and a detent protrusion configured to engage with the rocket, a first elastic body configured to elastically support the first end portion of the detent and connected to the first end portion, and an electrical safety device configured to prevent rotation of the detent including a hinge fixing frame having a hinge axis parallel to the detent rotation axis, a detent support configured to rotate around the hinge axis and support the detent, a hinge axis shaft arranged on the hinge axis, a solenoid configured to rotate the detent support by pushing the detent support, and a micro switch activated when the detent support rotates.


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    Titel :

    DUAL DETENT APPARATUS FOR ROCKET


    Beteiligte:
    LEE JUNHO (Autor:in) / BAE MINJI (Autor:in) / KIM YOUNGIL (Autor:in) / JEONG SORA (Autor:in)

    Erscheinungsdatum :

    13.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    DUAL DETENT APPARATUS FOR ROCKET

    LEE JUN HO / BAE MIN JI / KIM YOUNG IL et al. | Europäisches Patentamt | 2024

    Freier Zugriff

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    Rocket Detent and Release Mechanism

    B. H. Campbell / E. J. DeBona / W. J. Laird | NTIS | 1978


    Rocket Detent and Release Mechanism

    B. H. Campbell / E. J. Debona / W. J. Laird | NTIS | 1978