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    Integrated Cryptographic Circuits in Space Applications
    1.
    发明申请
    Integrated Cryptographic Circuits in Space Applications 有权

    公开(公告)号：US20220188428A1

    公开(公告)日：2022-06-16

    申请号：US17549752

    申请日：2021-12-13

    申请人： Tethers Unlimited, Inc.

    发明人： Sage Secilmis ,  Brad Mahlen ,  Dylan Del Castillo ,  Nat Zhurakovskyy ,  Jesse Cirillo

    IPC分类号： G06F21/60 ,  G06F21/72 ,  G06F21/82 ,  G06F11/30

    摘要： Cryptographic integrated circuits include an input module configured to receive a stream of input data packets, a plurality of cryptographic modules coupled to the input module, where each cryptographic module includes an input port for receiving an input data packet and an output port for transmitting an output data packet, and is configured to encrypt or decrypt the received input data packet to generate an output data packet, and an output module configured to receive output data packets from the plurality of cryptographic modules and to generate an output data stream comprising the output data packets, where the input and output modules and the plurality of cryptographic modules are mounted on a single integrated circuit board, and wherein the input module is configured to distribute the input data packets among the plurality of cryptographic modules.

    Electrodynamic tether and method of use
    3.
    发明授权
    Electrodynamic tether and method of use 失效
    电动系绳及其使用方法

    公开(公告)号：US6116544A

    公开(公告)日：2000-09-12

    申请号：US929271

    申请日：1997-09-12

    申请人： Robert L. Forward ,  Robert P. Hoyt

    发明人： Robert L. Forward ,  Robert P. Hoyt

    IPC分类号： B64G1/10 ,  B64G1/24 ,  B64G1/32 ,  B64G1/36 ,  B64G1/40 ,  B64G1/42 ,  B64G1/62 ,  B64G1/64 ,  B64G1/00

    CPC分类号： B64G1/421 ,  B64G1/10 ,  B64G1/24 ,  B64G1/32 ,  B64G1/36 ,  B64G1/40 ,  B64G1/62 ,  B64G1/648 ,  B64G1/242

    摘要： The present invention comprises an electrodynamic tether structure and a method of use. The structure of the tether taught by the present invention is a short, wide, interconnected multiwire (compared to the long, narrow single wires of the prior art) conductive tether whose area maximizes electrodynamic drag while simultaneously minimizing the Area-Time-Product swept by the tether during its operating life. The preferred tether length is two kilometers to five kilometers. The preferred tether mass is one percent to five percent of the spacecraft mass. The method of operation comprises orienting the tether structure at an angle to the local vertical to maximize electrodynamic drag on the host spacecraft and minimize tether instability. The angle of 35.26 degrees is preferred.

    摘要翻译： 本发明包括电动链系结构和使用方法。 本发明教导的系绳的结构是短的，宽的互连的多线（与现有技术的长而窄的单根导线相比），其面积最大化电动力阻力，同时最小化被扫描的面积时间产物 系绳在其使用寿命期间。 优选的系绳长度为两公里至五公里。 优选的系绳质量是飞船质量的百分之一至百分之五。 操作方法包括将系绳结构定位成与局部垂直方向成一定角度，以最大程度地使主机航天器上的电动力阻力最大化并最小化系绳不稳定性。 优选角度为35.26度。

    Launchable Tethered Remote Anchoring Module
    4.
    发明申请
    Launchable Tethered Remote Anchoring Module 审中-公开

    公开(公告)号：US20170121927A1

    公开(公告)日：2017-05-04

    申请号：US15340980

    申请日：2016-11-01

    申请人： Robert Hoyt

    发明人： Robert Hoyt

    IPC分类号： E02D5/80

    CPC分类号： E02D5/803 ,  E02D5/801 ,  E02D2600/10 ,  E02D2600/30

    摘要： A launchable land anchor having a tether, an anchor head housing a self-righting control module, a ground penetration device, a plurality of stability panels extending from a bottom portion having an interior surface and an exterior surface, and a plurality of sensors disposed on said exterior surface of said stability panels. Embodiments according to the present invention allow for self-righting functionality and continuous monitoring of stability to ensure security of the anchoring and removing the need of an on-site operator to setup and monitor the land anchor.

    Orbital winch
    5.
    发明授权
    Orbital winch 有权
    轨道绞车

    公开(公告)号：US09238572B2

    公开(公告)日：2016-01-19

    申请号：US14217434

    申请日：2014-03-17

    申请人： Robert Hoyt ,  Jeffrey T. Slostad ,  Scott Frank ,  Ian M. Barnes

    发明人： Robert Hoyt ,  Jeffrey T. Slostad ,  Scott Frank ,  Ian M. Barnes

    IPC分类号： B66D1/26 ,  B66D1/38

    CPC分类号： B66D1/38

    摘要： Orbital winch having: lower and upper frames; spool having upper and lower flanges with lower flange attached to lower frame; axial tether guide mounted to upper frame; secondary slewing ring coaxial with spool and rotatably mounted to upper frame, wherein secondary slewing ring's outer surface has gearing; upper tether guide mounted to inner surface of secondary slewing ring; linear translation means having upper end mounted to upper frame and lower end mounted on lower frame; primary slewing ring rotatably mounted within linear translation means allowing translation axially between flanges, wherein primary slewing ring's outer surface has gearing; lower tether guide mounted on primary slewing ring's inner surface; pinion rod having upper end mounted to upper frame and lower end mounted to lower frame, wherein pinion rod's teeth engage primary and secondary slewing rings' outer surface teeth; and tether passing through axial, upper, and lower tether guides and winding around spool.

    摘要翻译： 轨道绞车有：下框架和上框架; 阀芯具有上法兰和下法兰，下凸缘连接到下框架; 轴向导杆安装在上框架上; 副回转支承环与阀芯同轴并可旋转地安装在上框架上，其中次回转环的外表面具有齿轮传动; 上部系绳导轨安装在次级回转支承的内表面上; 线性平移装置，其上端安装到上框架，下端安装在下框架上; 主回转环可旋转地安装在线性平移装置内，允许在凸缘之间轴向平移，其中主回转支承件的外表面具有齿轮传动; 下部系链导轨安装在主回转支承的内表面上; 小齿轮杆，其上端安装到上框架，下端安装到下框架，其中小齿轮杆的齿啮合初级和次级回转环的外表面齿; 并且系绳穿过轴向，上部和下部系绳引导件并缠绕在卷轴上。

    METHODS AND APPARATUS FOR MANUFACTURE AND IN-SPACE ASSEMBLY OF ANTENNAS
    8.
    发明申请
    METHODS AND APPARATUS FOR MANUFACTURE AND IN-SPACE ASSEMBLY OF ANTENNAS 审中-公开

    公开(公告)号：US20190027835A1

    公开(公告)日：2019-01-24

    申请号：US16069510

    申请日：2017-01-11

    申请人： Tethers Unlimited Inc.

    发明人： Robert Hoyt

    IPC分类号： H01Q21/00 ,  H01Q3/26 ,  H01Q19/19 ,  H01Q1/28

    摘要： Apparatus for Manufacture and In-Space Assembly of Antennas comprising: a prefabricated primary reflector center section; a trusselator truss assembler; a phased feed array; wherein said prefabricated reflector center section, trusselator, and phased feed array are fixedly connected to one another; a self-positioning and orienting tool; a truss extending from said trusselator; a secondary reflector attached to said truss; robotic arms; a nibbler end effector mounted on one of said robotic arms; a grapple end effector mounted on one of said robotic arms; a mold for casting a piece of a primary reflector; a power cube; a solar array providing power to said power cube; refabricator plus; and an ESPA ring