Set of windows for space capsule
    1.
    外观设计

    公开(公告)号:USD1035548S1

    公开(公告)日:2024-07-16

    申请号:US29722958

    申请日:2020-02-03

    摘要: FIG. 1 is a perspective view of a set of windows for a space capsule according to the herein disclosed design.
    FIG. 2 is top-down view of the set of windows for a space capsule.
    FIG. 3 is a bottom-up view of the set of windows for a space capsule.
    FIG. 4 is a first side of the set of windows for a space capsule.
    FIG. 5 is a second side view of the set of windows for a space capsule shown rotated on a central axis 180 degrees relative to FIG. 4.
    FIG. 6 is a third side view of the set of windows for a space capsule shown rotated on a central axis 90 degrees counter-clockwise relative to FIG. 4; and,
    FIG. 7 is a fourth side view of the set of windows for a space capsule shown rotated on a central axis 90 degrees clockwise relative to FIG. 4.
    The broken lines showing of the space capsule in the drawings depicts environment only which forms no part of the claimed design.

    AEROSPACE VEHICLE SYSTEM AND METHOD OF OPERATION

    公开(公告)号:US20210331778A1

    公开(公告)日:2021-10-28

    申请号:US17370467

    申请日:2021-07-08

    IPC分类号: B64B1/40 B64D11/00

    摘要: An aerospace vehicle system, preferably including one or more capsules, and optionally including one or more propulsion modules and/or safety modules. A capsule, preferably including a pressure vessel including a structural frame and one or more windows, and optionally including a cabin. In alternate embodiments, the system can additionally or alternatively function as a terrestrial vehicle, a watercraft, and/or any other suitable vehicle. A method of operation, preferably including operating the aerospace vehicle system in flight, while maintaining a pressure differential between the pressure vessel interior and an environment surrounding the system.

    VEHICLE CABIN CONDITIONING SYSTEMoi
    7.
    发明公开

    公开(公告)号:US20240140621A1

    公开(公告)日:2024-05-02

    申请号:US18409529

    申请日:2024-01-10

    IPC分类号: B64G1/50

    CPC分类号: B64G1/50

    摘要: The cabin conditioning system can include a cabin air loop, a refrigerant loop, and a set of thermal rejection components. The system can optionally include a phase-change fluid loop. However, the cabin conditioning system can additionally or alternatively include any other suitable set of components. The cabin conditioning system functions to condition a cabin interior (and/or an air volume therein) of a vehicle, such as an atmospheric and/or space-flight capsule. Additionally or alternatively, the system can function to reject heat from the vehicle interior and/or vehicle power systems (e.g., avionics components thereof). Additionally or alternatively, the system can function to maintain the humidity of air within the cabin interior. However, the cabin conditioning system can include any other suitable components.