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    Method for performing exo-atmospheric missile's interception trial
    32.
    发明授权
    Method for performing exo-atmospheric missile's interception trial 有权

    公开(公告)号：US10260844B2

    公开(公告)日：2019-04-16

    申请号：US15130526

    申请日：2016-04-15

    申请人： ISRAEL AEROSPACE INDUSTRIES LTD.

    发明人： Jacob Rovinsky ,  Yoav Tourgeman

    IPC分类号： F41J2/00 ,  F42B10/60 ,  F42B10/62 ,  F41J2/02 ,  F41G7/00 ,  F41J9/08 ,  F42B8/12 ,  F42B8/24 ,  F41J9/00

    摘要： There is provided an inflatable dummy target comprising a chassis wrapped with a sheet. The chassis can be formed by individual inflatable ducts and can comprise at least two ring-shaped ducts interconnected by one or more elongate ducts. The inflatable dummy target can further comprise rigidizing ducts. The inflatable dummy target geometry can be conical, cylindrical, etc. Optionally, the inflatable dummy target can comprise several attached axi-symmetrical sections, wherein each section has a chassis wrapped with a sheet, the chassis formed by individual inflatable ducts. Optionally, the shape of each section can be selected from the group consisting of conical, frustoconical and cylindrical forms.

    Rocket-deployed balloon for position marker
    34.
    发明授权
    Rocket-deployed balloon for position marker 失效
    火箭部署的气球用于位置标记

    公开(公告)号：US3930448A

    公开(公告)日：1976-01-06

    申请号：US495479

    申请日：1974-08-07

    申请人： William H. Barber ,  Werner F. Beckert ,  Ottmar H. Dengel

    发明人： William H. Barber ,  Werner F. Beckert ,  Ottmar H. Dengel

    IPC分类号： F42B8/24 ,  F42B12/36 ,  F42B12/68 ,  F42B13/42

    CPC分类号： F42B12/68 ,  F42B12/36 ,  F42B8/24

    摘要： A portable, rocket-deployed signaling system for deploying a pin-point loion marker including a tractor rocket propulsion unit and attached payload container launched from a hand-held tube. The payload comprises an inflatable marker balloon, a gas generator for inflating the balloon and a tether line connecting the balloon to the launcher tube. A coupling pin, secured to the tether line at a predetermined length from the end attached to the launcher tube and removably supported on the payload container, is pulled subsequent to launch to permit the container to separate and deploy the balloon. A percussion igniter then actuates the gas generator to inflate the balloon with the generator separating after inflation.

    摘要翻译： 一种便携式，火箭部署的信号系统，用于部署包括从手持管发射的拖拉机火箭推进单元和附着的有效载荷容器的针尖位置标记。 有效载荷包括可充气标记气球，用于使球囊充气的气体发生器和将球囊连接到发射管的系绳。 从连接到发射管的一端以预定长度固定到系绳的连接销被可拆卸地支撑在有效载荷容器上，在发射之后被拉动以允许容器分离和展开气囊。 然后，敲击点火器在充气之后致动气体发生器以使发生器分离的气囊膨胀。

    Model rocket-glider
    35.
    发明授权
    Model rocket-glider 失效
    模型火箭滑翔机

    公开(公告)号：US3888178A

    公开(公告)日：1975-06-10

    申请号：US51919274

    申请日：1974-10-30

    申请人： SENOSKI WALTER E

    发明人： SENOSKI WALTER E

    IPC分类号： F42B8/24 ,  F42B15/16 ,  A63H27/06

    CPC分类号： F42B8/24

    摘要： A solid fuel-powered model rocket having a main body tube and at least one auxiliary body tube. A solid fuel motor is mounted in the after end of one of the tubes and a slidable plug is disposed in the after end of the other tube, the plug being provided with a latch for engaging a wing elevator and maintaining it parallel to the horizontal plane of the wing against the biasing of a resilient band while the craft is in vertical flight. Following burn-out of the propellant charge, the gases generated upon ignition of a blow-out charge in the fuel cartridge cause rearward displacement of the slidable plug, disengagement of the latch and deployment of the elevator to a predetermined up-angel relative to the top horizontal plane of the wing, thereby directing the craft into a generally horizontal glide attitude.

    摘要翻译： 一种固体燃料动力型火箭，其具有主体管和至少一个辅助体管。 固体燃料电动机安装在其中一个管的后端，并且可滑动的塞子设置在另一个管的后端，插头设置有用于接合机翼升降机并保持其平行于水平面的闩锁 的机翼抵抗弹性带的偏压，同时飞行器处于垂直飞行。 在燃料喷射燃料燃烧之后，燃料筒中的吹出电荷点火时产生的气体引起滑动插头向后的位移，闩锁的分离和电梯的展开相对于预定的上升天使 机翼的顶部水平面，从而将飞行物引导到大体上水平的滑翔姿态。