SOLAR SAIL ATTACHMENT AND DEPLOYMENT METHODS

    公开(公告)号:US20220388694A1

    公开(公告)日:2022-12-08

    申请号:US17453333

    申请日:2020-05-04

    申请人: L'Garde, Inc.

    IPC分类号: B64G1/40 B64G1/22

    摘要: Exemplary embodiments provided herein include an attachment and deployment system and method. Exemplary embodiments may use features together or separately as desired. The attachment feature may be used to periodically couple a solar sail.

    SPACE DEBRIS ENGAGEMENT AND DEORBIT SYSTEM

    公开(公告)号:US20220127020A1

    公开(公告)日:2022-04-28

    申请号:US17468472

    申请日:2021-09-07

    申请人: L'GARDE, INC.

    摘要: Exemplary embodiments described herein include innovative engagement devices. Exemplary engagement devices may include on or more tape spring systems. The tape spring system may include a continuous or segmented bi-stable tape spring. The tape spring can be stowed in a rolled up configuration, extended to a deployed configuration, and then triggered to return to a retracted configuration.

    Compactable RF Membrane Antenna
    3.
    发明申请

    公开(公告)号:US20190097300A1

    公开(公告)日:2019-03-28

    申请号:US16080977

    申请日:2017-02-28

    申请人: L'Garde, Inc.

    IPC分类号: H01Q1/08 H01Q15/16 H01Q1/28

    摘要: Exemplary embodiments are described herein for compactable antennas. Exemplary compactable antennas include a support structure and a reflector surface. The support structure may directly or indirectly define the reflector shape. Exemplary embodiments comprise deployable support structures to permit the compactable antenna to have a smaller volume stowed configuration and a larger volume deployed configuration.

    SPACE DEBRIS ENGAGEMENT AND DEORBIT SYSTEM
    9.
    发明申请

    公开(公告)号:US20200377239A1

    公开(公告)日:2020-12-03

    申请号:US16277944

    申请日:2019-02-15

    申请人: L'GARDE, INC.

    摘要: Exemplary embodiments described herein include innovative engagement devices. Exemplary engagement devices may include on or more tape spring systems. The tape spring system may include a continuous or segmented bi-stable tape spring. The tape spring can be stowed in a rolled up configuration, extended to a deployed configuration, and then triggered to return to a retracted configuration.

    Rocket Morphing Aerial Vehicle
    10.
    发明申请
    Rocket Morphing Aerial Vehicle 审中-公开
    火箭变形飞行器

    公开(公告)号:US20160046372A1

    公开(公告)日:2016-02-18

    申请号:US14722104

    申请日:2015-05-26

    申请人: L'Garde, Inc.

    IPC分类号: B64C39/02 B64D17/80 B64F1/10

    摘要: A rocket morphing aerial vehicle has a first rocket configuration and a second aerial vehicle configuration. The rocket morphing aerial vehicle may be used to deploy an aerial vehicle at further distances faster. The rocket configuration may be used to get the aerial vehicle to its desired location, while the aerial vehicle is used for the desired task. The rocket morphing aerial vehicle may include a deceleration mechanism such that the speed of the rocket does not interfere with the deployment of the aerial vehicle.

    摘要翻译: 火箭变形飞行器具有第一火箭构型和第二空中飞行器构造。 火箭变形飞行器可以用于更快地部署更远的飞行器。 可以使用火箭配置来将空中飞行器用于所需的位置,而空中飞行器则用于所需的任务。 火箭变形飞行器可以包括减速机构,使得火箭的速度不会干扰飞行器的展开。