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1. 发明申请

US20090140100A1 REUSABLE ORBITAL VEHICLE WITH INTERCHANGEABLE CARGO MODULES 审中-公开
标题翻译：具有可交换货物模块的可重复使用的轨道车辆
公开(公告)号：US20090140100A1
公开(公告)日：2009-06-04
申请号：US12324746
申请日：2008-11-26
申请人： George E. Mueller , Richard H. Kohrs , William B. Duncan , David B. Cochran , Dean L. Misterek , Terrill L. Burlison , Ryan M. Curtis , Thomas Johnson , Richard A. Bailey , Charles D. Limerick
发明人： George E. Mueller , Richard H. Kohrs , William B. Duncan , David B. Cochran , Dean L. Misterek , Terrill L. Burlison , Ryan M. Curtis , Thomas Johnson , Richard A. Bailey , Charles D. Limerick
IPC分类号： B64G1/00
CPC分类号： B64G1/14 , B64G2001/1092
摘要： A reusable module is affixed atop a reusable orbital vehicle (OV). Various configurations of the reusable module have identical external dimensions in the region of attachment to the OV to permit interchangeability. Different configurations can accommodate a variety of missions of different type and duration. A variety of cargo modules of different configurations allow cargo to be uplifted into orbit. In one embodiment, the cargo module is an unpressurized cargo module in which the cargo is exposed to the environment of space during the unloading process. The cargo module may also be a pressurized cargo module. In an alternative embodiment, the cargo module may include both a pressurized cargo module and unpressurized cargo module.
摘要翻译：可重复使用的模块固定在可重复使用的轨道车辆（OV）上。可再利用模块的各种配置在连接到OV的区域中具有相同的外部尺寸以允许可互换性。不同的配置可以适应不同类型和持续时间的各种任务。不同配置的各种货物模块可以将货物提升到轨道上。在一个实施例中，货物模块是非加压货物模块，其中货物在卸载过程中暴露于空间环境中。货物模块也可以是加压货物模块。在替代实施例中，货物模块可以包括加压货物模块和非加压货物模块。

2. 发明授权

US07198233B1 Reusable orbital vehicle with interchangeable cargo modules 失效
标题翻译：具有可互换货物模块的可重复使用的轨道车辆
公开(公告)号：US07198233B1
公开(公告)日：2007-04-03
申请号：US11230051
申请日：2005-09-19
申请人： George E. Mueller , Richard H. Kohrs , William B. Duncan , David B. Cochran , Dean L. Misterek , Terill L. Burlison , Ryan M. Curtis , Thomas Johnson , Richard A. Bailey , Charles D. Limerick
发明人： George E. Mueller , Richard H. Kohrs , William B. Duncan , David B. Cochran , Dean L. Misterek , Terill L. Burlison , Ryan M. Curtis , Thomas Johnson , Richard A. Bailey , Charles D. Limerick
IPC分类号： F03H5/00
CPC分类号： B64G1/14 , B64G2001/1092
摘要： A reusable module is affixed atop a reusable orbital vehicle (OV). Various configurations of the reusable module have identical external dimensions in the region of attachment to the OV to permit interchangeability. Different configurations can accommodate a variety of missions of different type and duration. A variety of cargo modules of different configurations allow cargo to be uplifted into orbit. In one embodiment, the cargo module is an unpressurized cargo module in which the cargo is exposed to the environment of space during the unloading process. The cargo module may also be a pressurized cargo module. In an alternative embodiment, the cargo module may include both a pressurized cargo module and unpressurized cargo module.
摘要翻译：可重复使用的模块固定在可重复使用的轨道车辆（OV）上。可再利用模块的各种配置在连接到OV的区域中具有相同的外部尺寸以允许可互换性。不同的配置可以适应不同类型和持续时间的各种任务。不同配置的各种货物模块可以将货物提升到轨道上。在一个实施例中，货物模块是非加压货物模块，其中货物在卸载过程中暴露于空间环境中。货物模块也可以是加压货物模块。在替代实施例中，货物模块可以包括加压货物模块和非加压货物模块。

3. 发明申请

US20100051751A1 REUSABLE ORBITAL VEHICLE WITH INTERCHANGEABLE MODULES 审中-公开
标题翻译：具有可互换模块的可重复使用的轨道车辆
公开(公告)号：US20100051751A1
公开(公告)日：2010-03-04
申请号：US12615892
申请日：2009-11-10
申请人： George E. Mueller , Richard H. Kohrs , Dean L. Misterek , David B. Cochran , William B. Duncan , Charles D. Limerick
发明人： George E. Mueller , Richard H. Kohrs , Dean L. Misterek , David B. Cochran , William B. Duncan , Charles D. Limerick
IPC分类号： B64G1/60 , B64G1/24 , B64G1/64 , B64G1/46 , B64G1/52 , B64G1/66
CPC分类号： B64G1/14 , B64G1/52 , B64G1/60 , B64G1/646
摘要： A reusable module is affixed atop a reusable orbital vehicle (OV). Various configurations of the reusable module have identical external dimensions in the region of attachment to the OV, aerodynamic characteristics, and mounting configurations to permit interchangeability. Different configurations can accommodate a variety of missions of different type and duration. The module may be a cargo module, a satellite payload module or a passenger module. The passenger module is provided in a variety of configurations to accommodate a different number of passengers and cargo based on mission parameters.
摘要翻译：可重复使用的模块固定在可重复使用的轨道车辆（OV）上。可再利用模块的各种构造在与OV的连接区域，空气动力学特性以及安装构造中具有相同的外部尺寸以允许可互换性。不同的配置可以适应不同类型和持续时间的各种任务。模块可以是货物模块，卫星有效载荷模块或乘客模块。乘客模块以各种配置提供，以根据任务参数来容纳不同数量的乘客和货物。

4. 发明授权

US06513760B1 Logistics module system and method 失效
标题翻译：物流模块系统及方法
公开(公告)号：US06513760B1
公开(公告)日：2003-02-04
申请号：US09735201
申请日：2000-12-11
申请人： George E. Mueller , Richard H. Kohrs , David B. Cochran , Joseph W. Cuzzupoli , Charles D. Limerick , Richard A. Bailey , Thomas G. Johnson , Steven C. Knowles
发明人： George E. Mueller , Richard H. Kohrs , David B. Cochran , Joseph W. Cuzzupoli , Charles D. Limerick , Richard A. Bailey , Thomas G. Johnson , Steven C. Knowles
IPC分类号： F03H500
CPC分类号： B64G1/646 , B64G1/002 , B64G1/1078 , B64G1/12 , B64G1/401 , B64G1/62 , B64G1/641
摘要： An orbital vehicle (34) having a propulsion module (33) and a logistics module (36). The logistics module includes a generally cylindrical outer shell (56, 541, 542) with first and second ends. An openable cover (58) is coupled with the outer shell at the first end, thereby providing access to the interior of the logistics module. The second end is adapted to couple to the propulsion module. A cargo container (54) is disposed generally within the outer shell, the cargo container including a berthing mechanism (70) disposed to be accessible when the cover is opened. A retractable grapple fixture (176) is provided on the logistics module, selectively positionable between an extended position and a retracted position. When the grapple fixture is in the extended position a grapple shaft (78) can be accessed to secure the orbital vehicle. When the grapple fixture is retracted, it is enclosed within the orbital vehicle.
摘要翻译：具有推进模块（33）和物流模块（36）的轨道车辆（34）。后勤模块包括具有第一端和第二端的大致圆柱形外壳（56,541,542）。可开启盖（58）在第一端与外壳结合，从而提供进入物流模块内部的通路。第二端适于联接到推进模块。货物集装箱（54）通常设置在外壳内，货物集装箱包括设置成当盖打开时可接近的停泊机构（70）。在物流模块上设置有可伸缩抓斗夹具（176），其可选择性地定位在延伸位置和缩回位置之间。当抓斗固定装置处于伸出位置时，抓斗轴（78）可以被接近以固定轨道车辆。当抓斗夹具缩回时，它被包围在轨道车辆内。

5. 发明授权

US06789767B2 Active satellite dispenser for reusable launch vehicle 失效
标题翻译：主动卫星分配器可重复使用的运载火箭
公开(公告)号：US06789767B2
公开(公告)日：2004-09-14
申请号：US10132083
申请日：2002-04-23
申请人： George E. Mueller , David B. Cochran , Richard H. Kohrs
发明人： George E. Mueller , David B. Cochran , Richard H. Kohrs
IPC分类号： B64G164
CPC分类号： B64G1/26 , B64G1/007 , B64G1/1085 , B64G1/222 , B64G1/641 , B64G1/645
摘要： An active satellite dispenser is preferably attachable to a reusable launch vehicle for deployment of one or more satellites into one or more desired orbits. The active satellite dispenser includes a center mast that releasably receives the satellite(s), a liquid propellant rocket, and an orbital control system on an avionics pallet. In the preferred embodiment, a pressurized gas selectively pressurizes the propellant tanks (which may include fuel and oxidizer tanks), to provide propellant to the rocket. In operation, the launch vehicle releases the satellite dispenser in a first deployment orbit. The active dispenser rocket and orbital control system then transport the active dispenser and satellite(s) into the final deployment orbit. In the preferred embodiment the active dispenser can operate multiple times to place individual satellites in different orbits.
摘要翻译：主动卫星分配器优选地可附接到可重复使用的运载火箭上，用于将一个或多个卫星部署到一个或多个所需轨道中。主动卫星分配器包括可释放地接收卫星的中心桅杆，液体推进剂火箭和航空电子托盘上的轨道控制系统。在优选实施例中，加压气体选择性地使推进剂罐（其可以包括燃料和氧化剂罐）加压，以向火箭提供推进剂。在运行中，运载火箭在第一部署轨道上释放卫星分配器。主动分配器火箭和轨道控制系统然后将主动分配器和卫星运送到最终部署轨道。在优选实施例中，主动分配器可以多次操作以将各个卫星放置在不同的轨道中。

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