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    EXTENDABLE CONDUCTOR FOR THERMAL MANAGEMENT
    2.
    发明申请
    EXTENDABLE CONDUCTOR FOR THERMAL MANAGEMENT 审中-公开

    公开(公告)号：WO2023070001A1

    公开(公告)日：2023-04-27

    申请号：PCT/US2022/078383

    申请日：2022-10-19

    申请人： LUNAR OUTPOST INC.

    发明人： GEMER, Andrew, Josef ,  MOXHAM, Colby ,  WAGNER, Van ,  WILSON, Peter

    IPC分类号： B64G1/16 ,  F28D21/00 ,  E21B7/24 ,  E21C51/00

    摘要： Aspects of the present disclosure relate to an extendable conductor assembly. A conductor of the extendable conductor assembly may be extended (e.g., into a thermal target, such as a preexisting or a newly created feature of a planetary body) and used to thermally couple a rover, vehicle, fixed installation, or other hardware with the thermal target. Thus, the temperature of the hardware may be managed via heat transfer to/from the thermal target. For instance, heat may be transferred from the thermal target to maintain the temperature of the hardware under cold conditions, while excess heat may be transferred to the thermal target under hot conditions. As an example, a rover may form a borehole in the lunar surface, in which a conductor may be extended to facilitate heat transfer between the rover and the Moon accordingly.

    DISPOSITIF DE CONTRÔLE DE VITESSE ANGULAIRE D'UN ENGIN SPATIAL ET ENGIN SPATIAL CORRESPONDANT
    4.
    发明申请
    DISPOSITIF DE CONTRÔLE DE VITESSE ANGULAIRE D'UN ENGIN SPATIAL ET ENGIN SPATIAL CORRESPONDANT 审中-公开

    公开(公告)号：WO2023047049A1

    公开(公告)日：2023-03-30

    申请号：PCT/FR2022/051767

    申请日：2022-09-20

    申请人： AIRBUS DEFENCE AND SPACE SAS

    发明人： BOYER, Laurent ,  LAGADEC, Kristen

    IPC分类号： B64G1/32 ,  B64G1/24

    摘要： Dispositif de contrôle de vitesse angulaire d'un engin spatial et engin spatial correspondant L'invention concerne un dispositif (1) de contrôle de vitesse angulaire d'un engin (2) spatial hors service permettant de faciliter les opérations de retrait actif de l'engin spatial en tant que débris spatial. Un tel dispositif comprend un stator (3) et un rotor (4) mobile selon un axe (A21) de rotation par rapport au stator, le stator (3) étant destiné à être entrainé par l'engin (2) spatial à stabiliser, le rotor (4) étant destiné à s'orienter selon le champ (5) magnétique terrestre. Le stator (3) comprend un corps (6) électriquement conducteur et non-ferromagnétique tandis que le rotor (4) comprend un système aimanté (7) configuré pour induire, dans le stator (3), des courants de Foucault de freinage d'un mouvement relatif du rotor (4) par rapport au stator (3).

    SATELLITE AND ANTENNA THEREFOR
    5.
    发明申请
    SATELLITE AND ANTENNA THEREFOR 审中-公开

    公开(公告)号：WO2023044162A1

    公开(公告)日：2023-03-23

    申请号：PCT/US2022/044139

    申请日：2022-09-20

    申请人： WILDSTAR, LLC

    发明人： WYLER, Gregory Thane ,  HOLDEN, Bobby Glenn ,  SWEENEY, Katelyn

    IPC分类号： B64G1/10 ,  B64G1/22 ,  B64G1/66 ,  H01Q1/28 ,  B64G1/32

    摘要： A satellite in accordance with the present teachings has plural "thin" (i.e., panel-like) segments, which are coupled together and extendable along the in-track direction of movement of the satellite. One or more of these segments, which is advantageously an antenna panel, has the ability to "roll" relative other segments. This enables the satellite to establish and maintain direct pointing of the antenna panel to a targeted area on the ground. The antenna panel includes linear, electronically steerable array.

    測位方法、月測位システム、および、測位衛星
    8.
    发明申请
    測位方法、月測位システム、および、測位衛星 审中-公开

    公开(公告)号：WO2023032822A1

    公开(公告)日：2023-03-09

    申请号：PCT/JP2022/032122

    申请日：2022-08-25

    申请人： 三菱電機株式会社

    发明人： 迎　久幸

    IPC分类号： B64G1/10 ,  B64G1/24 ,  B64G1/66 ,  B64G3/00

    摘要： 飛翔体（５００）は、地球から月または惑星に向かう宇宙空間ないし月または惑星の近傍を飛翔する。飛翔体（５００）は、測位信号受信装置を具備する。地上局（１００）は、指向方向制御機能付き測位信号送信装置を具備し、地球固定座標系における位置座標が既知である。飛翔体（５００）は、地上局（１００）から送信する測位信号（２１）を、同時に４か所の地上局（１００）から受信して、地球固定座標系における位置座標を計測する。

    MODULAR CONFIGURATION OF LAUNCH VEHICLE SYSTEM
    9.
    发明申请
    MODULAR CONFIGURATION OF LAUNCH VEHICLE SYSTEM 审中-公开

    公开(公告)号：WO2023031967A1

    公开(公告)日：2023-03-09

    申请号：PCT/IN2022/050780

    申请日：2022-09-01

    申请人： AGNIKUL COSMOS PRIVATE LIMITED

    发明人： -, 'Syed Peer Mohamed Shah Khadri ,  RAVICHANDRAN, Srinath

    IPC分类号： B64G1/00 ,  B64G1/40

    摘要： The present invention relates to a modular configuration of the launch vehicle system. More specifically, it relates to the modular configuration technology developed to optimise the launch vehicle with respect to the number of engines in the lower stage or the number of stages itself in order to get a most efficient launch possible for a particular payload being launched. In the present invention the vehicle is such that the modularity is passed down to sub-system level which thereby reduces the mass of unused components and the modifiable cluster can be used as a booster unit to carry heavier payloads to higher orbits. Depending upon the mass of the payload to be carried to a particular orbit, either the number of stages or the number of engines (601, 602, 603, 604), are either attached or removed from the vehicle and thus increasing the efficiency of the trajectory. The present invention reduces the time and cost involved in reconfiguration as well.

    SAMPLE COLLECTION ASSEMBLY FOR A VEHICLE
    10.
    发明申请
    SAMPLE COLLECTION ASSEMBLY FOR A VEHICLE 审中-公开

    公开(公告)号：WO2023028500A1

    公开(公告)日：2023-03-02

    申请号：PCT/US2022/075369

    申请日：2022-08-23

    申请人： LUNAR OUTPOST INC.

    发明人： GEMER, Andrew Josef ,  CYRUS, Justin ,  WAGNER, Van ,  WILSON, Peter

    IPC分类号： B64G1/16 ,  G01N1/04

    摘要： Aspects of the present disclosure relate to a sample collection assembly for a vehicle. The sample collection assembly includes a perforated ground-engaging member of the vehicle and an associated sample collector. For example, a perforated wheel may collect material from terrain under the vehicle as the wheel rotates (e.g., as may result from movement of the vehicle), which may fall through the perforation and into a sample collector disposed thereunder. In some examples, a ground-engaging member may include one or more grousers, paddles, or scoops, among other terrain interaction features, to further increase the amount of material that is collected. Such terrain interaction features may be unidirectional or bidirectional, thereby offering improved sample collection in one or both directions of operation, respectively. In examples, an image capture device or one or more other sensors may be used to monitor sample collection and/or to process data associated therewith.