The present disclosure provides a payload deployment system that is operative to receive and retain a configurable payload. The payload deployment mechanism helps to reduce the drag of the payload and to protect the payload from environmental factors. The payload may be released using a hinge mechanism to ensure the payload does not contact the payload deployment mechanism when the payload is deployed. A vent may be utilized to equalize pressure between the external environment and a body portion of the payload deployment mechanism. The vent may generate an additional force to assist in separating the payload from the launcher.


    Access

    Download


    Export, share and cite



    Title :

    ROTATING RELEASE LAUNCHING SYSTEM



    Publication date :

    2023-08-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ROTATING RELEASE LAUNCHING SYSTEM

    ALLEY NICHOLAS ROBERT / WILLIAMS JESSE OWEN / BRASHER MATTHEW GORDON | European Patent Office | 2022

    Free access

    ROTATING RELEASE LAUNCHING SYSTEM

    ALLEY NICHOLAS ROBERT / WILLIAMS JESSE OWEN / BRASHER MATTHEW GORDON | European Patent Office | 2022

    Free access

    ROTATING RELEASE LAUNCHING SYSTEM

    ALLEY NICHOLAS ROBERT / WILLIAMS JESSE OWEN / BRASHER MATTHEW GORDON | European Patent Office | 2021

    Free access

    ROTATING RELEASE LAUNCHING SYSTEM

    ALLEY NICHOLAS ROBERT / WILLIAMS JESSE OWEN / BRASHER MATTHEW GORDON | European Patent Office | 2024

    Free access

    ROTATING RELEASE LAUNCHING SYSTEM

    ALLEY NICHOLAS ROBERT / WILLIAMS JESSE OWEN / BRASHER MATTHEW GORDON et al. | European Patent Office | 2023

    Free access