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公开(公告)号：US10012481B2
公开(公告)日：2018-07-03
申请号：US14861328
申请日：2015-09-22
发明人： Jacob Rovinsky , Yoav Tourgeman
摘要： An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.
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公开(公告)号：US4449939A
公开(公告)日：1984-05-22
申请号：US502404
申请日：1983-06-08
申请人： William R. Matteson
发明人： William R. Matteson
摘要： A safe-arm simulator device for use in training personnel in maintaining operating a missile rocket motor fuze safe-arm device of the type presently utilized on live missiles is disclosed. The device comprises a spring mounted on a rotatable shaft contained within a cylindrical housing. The housing is inserted in a bored hole of a dummy missile, exposing a key slot in the base of the shaft. A key is mounted on the device for turning the device from a safe to arm position. The spring offers resistance to turning similarly incurred in a live safe-arm device and likewise returns and maintains the device in a safe orientation unless locked in the arm position.
摘要翻译： 公开了一种用于培训人员维护和操作目前在活体导弹上使用的导弹火箭发动机引信安全臂装置的安全臂模拟装置。 该装置包括安装在容纳在圆柱形壳体内的可旋转轴上的弹簧。 将壳体插入虚拟导弹的钻孔中，露出轴的基座中的键槽。 一个钥匙安装在设备上，用于将设备从安全位置转移到手臂位置。 该弹簧提供了类似于在活安全臂装置中产生的转弯的阻力，并且同样地将装置保持在安全的方向，除非锁定在手臂位置。
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公开(公告)号：US3805355A
公开(公告)日：1974-04-23
申请号：US31551572
申请日：1972-12-15
申请人： GORNIK M
发明人： GORNIK M
CPC分类号： F42B10/06 , F41B5/1446 , F42B8/24 , Y10T29/53974
摘要： A fixture facilitating the accurate positioning and gluing of fins to the tubular body of a model rocket.
摘要翻译： 一种固定装置，有利于将翅片准确定位并粘贴到模型火箭的管状体上。
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公开(公告)号：US3086317A
公开(公告)日：1963-04-23
申请号：US1635060
申请日：1960-03-21
申请人： ALESSANDRO QUERCETTI
发明人： ALESSANDRO QUERCETTI
CPC分类号： A63H27/14 , A63H27/005 , F42B8/24
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公开(公告)号：US3081626A
公开(公告)日：1963-03-19
申请号：US5912160
申请日：1960-09-28
申请人： SHALLER HERMAN I
发明人： SHALLER HERMAN I
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公开(公告)号：US2960035A
公开(公告)日：1960-11-15
申请号：US76127258
申请日：1958-09-15
申请人： BURTON ROBERT W
发明人： BURTON ROBERT W
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公开(公告)号：US20170122705A1
公开(公告)日：2017-05-04
申请号：US15339011
申请日：2016-10-31
发明人： Jacob ROVINSKY , Yoav TOURGEMAN
CPC分类号： F41G7/002 , F41G7/003 , F41G7/004 , F41G7/006 , F41G7/30 , F41J2/02 , F41J9/08 , F42B8/24 , F42B12/58
摘要： An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet. The chassis of inflatable ducts can include one or more ring shaped ducts and one or more elongate ducts. The chassis can include at least two ring shaped ducts interconnected by one or more elongate ducts. The dummy target can include several attached axi-symmetrical sections, each section have a chassis of inflatable ducts. Each section can be conical, frustoconical or cylindrical, thereby achieving a concave or convex dummy target geometry.
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公开(公告)号：US4340197A
公开(公告)日：1982-07-20
申请号：US529182
申请日：1966-02-15
申请人： George S. Campbell
发明人： George S. Campbell
摘要： A decoy missile having a high moment of inertia with a corresponding reduction of the natural oscillation frequency for simulating reentry of a ballistic nose cone into the earth's atmosphere. High density ballast material disposed in the forward section is in proportional relationship to similar ballast material in the base section such that the distance between the center of pressure and the center of gravity is equal to one-half the base diameter.
摘要翻译： 具有高转动惯量的诱饵导弹，相应地降低了自然振荡频率，用于模拟弹道鼻锥重新进入地球大气层。 设置在前部的高密度压载材料与基部中类似的压载材料成比例关系，使得压力中心和重心之间的距离等于基础直径的一半。
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公开(公告)号：US3942441A
公开(公告)日：1976-03-09
申请号：US469438
申请日：1974-05-13
申请人： Walter E. Senoski
发明人： Walter E. Senoski
CPC分类号： F42B8/24
摘要： A model rocket, the nose cone of which is ejected clear of the rocket body after the rocket has spent its fuel, including means for replacing the ejected nose cone during flight with another nose cone and means for altering the configuration wing elevator during flight thereby converting the rocket to a glider.
摘要翻译： 一种示火箭，其火箭在火箭消耗燃料之后，其鼻锥在火箭弹身上弹出，包括用于在飞行期间用另一个鼻锥更换喷射的鼻锥的装置，以及用于在飞行过程中改变构型翼电梯的装置 火箭到滑翔机。
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