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公开(公告)号:US20240246491A1
公开(公告)日:2024-07-25
申请号:US18589037
申请日:2024-02-27
Applicant: BLUE ORIGIN, LLC
Inventor: Michael David Johnson
Abstract: A representative spacecraft system includes a launch vehicle elongated along a launch vehicle axis and having at least one stage carrying a corresponding rocket engine. The representative system further includes an annular support structure carried by the at least one stage and positioned to support a cargo spacecraft having a service module and a cargo module. The cargo module of the cargo spacecraft is positioned along the launch vehicle axis in a direction distal from the support structure, and at least a portion of the service module of the cargo spacecraft positioned within an annulus of the support structure.
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公开(公告)号:US11945406B2
公开(公告)日:2024-04-02
申请号:US18099192
申请日:2023-01-19
Applicant: Blue Origin, LLC
Inventor: Michael David Johnson
Abstract: A representative spacecraft system includes a launch vehicle elongated along a launch vehicle axis and having at least one stage carrying a corresponding rocket engine. The representative system further includes an annular support structure carried by the at least one stage and positioned to support a cargo spacecraft having a service module and a cargo module. The cargo module of the cargo spacecraft is positioned along the launch vehicle axis in a direction distal from the support structure, and at least a portion of the service module of the cargo spacecraft positioned within an annulus of the support structure.
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公开(公告)号:US11565628B2
公开(公告)日:2023-01-31
申请号:US16370660
申请日:2019-03-29
Applicant: Blue Origin, LLC
Inventor: Michael David Johnson
Abstract: A representative spacecraft system includes a launch vehicle elongated along a launch vehicle axis and having at least one stage carrying a corresponding rocket engine. The representative system further includes an annular support structure carried by the at least one stage and positioned to support a cargo spacecraft having a service module and a cargo module. The cargo module of the cargo spacecraft is positioned along the launch vehicle axis in a direction distal from the support structure, and at least a portion of the service module of the cargo spacecraft positioned within an annulus of the support structure.
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公开(公告)号:US20200307461A1
公开(公告)日:2020-10-01
申请号:US16370660
申请日:2019-03-29
Applicant: Blue Origin, LLC
Inventor: Michael David Johnson
Abstract: Spacecraft with increased cargo capacities, and associated systems and methods are disclosed, A representative spacecraft system includes a launch vehicle elongated along a launch vehicle axis and having at least one stage carrying a corresponding rocket engine. The representative system further includes an annular support structure carried by the at least one stage and positioned to support a cargo spacecraft having a service module and a cargo module. The cargo module of the cargo spacecraft is positioned along the launch vehicle axis in a direction distal from the support structure, and at least a portion of the service module of the cargo spacecraft positioned within an annulus of the support structure
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公开(公告)号:US20230202399A1
公开(公告)日:2023-06-29
申请号:US18099192
申请日:2023-01-19
Applicant: Blue Origin, LLC
Inventor: Michael David Johnson
Abstract: A representative spacecraft system includes a launch vehicle elongated along a launch vehicle axis and having at least one stage carrying a corresponding rocket engine. The representative system further includes an annular support structure carried by the at least one stage and positioned to support a cargo spacecraft having a service module and a cargo module. The cargo module of the cargo spacecraft is positioned along the launch vehicle axis in a direction distal from the support structure, and at least a portion of the service module of the cargo spacecraft positioned within an annulus of the support structure
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