公开(公告)号：WO2023282948A2

公开(公告)日：2023-01-12

申请号：PCT/US2022/024273

申请日：2022-04-11

Applicant: SIERRA SPACE CORPORATION

Inventor： WOODS, Grant, Robert ,  HICKERSON, Jeffrey, S. ,  SANDY, Charles, Ralph

IPC: B64G1/60 ,  B64G1/12 ,  B64G1/646 ,  B64G2001/224 ,  B64G99/00

Abstract: Methods, devices, and systems are described for a bracket fixture for securing a load to a soft goods layer in a space habitat. The bracket fixture includes a base having a plurality of sides, the plurality of sides having a pin parallel to its respective side, and an aperture between the pin and the respective side. The bracket fixture further includes a protrusion extending from the base, the protrusion including a fixture element.

公开(公告)号：WO2020077247A1

公开(公告)日：2020-04-16

申请号：PCT/US2019/055914

申请日：2019-10-11

Applicant: BLOXTON INVESTMENT GROUP, LLC

Inventor： BLOXTON, Michael

IPC: B64G1/12 ,  B64G1/00 ,  B64G1/64 ,  B64G1/10 ,  B64G1/22 ,  B64G1/60 ,  B64G99/00

Abstract: A space station includes: a core with multiple connected core pods; a ring with multiple connected ring pods; at least one shaft connecting the core and the ring, the at least one shaft including multiple connected shaft pods. The core pods are substantially identical to one another, the ring pods are substantially identical to one another, and the shaft pods are substantially identical to one another.

公开(公告)号：WO2019018086A1

公开(公告)日：2019-01-24

申请号：PCT/US2018/037655

申请日：2018-06-14

Applicant: THE AEROSPACE CORPORATION

Inventor： HELVAJIAN, Henry

IPC: B64G1/12 ,  B64G1/22 ,  B64G1/64 ,  B64G99/00 ,  B64G1/66

Abstract: Cell-based space systems with nested-ring structures that interlock and can change configuration to support a mission are provided. The cells may self-assemble into a larger structure to carry out a mission. Multiple rotatable rings may be included in a cell, with a payload/control section in the center. The rings may provide power and/or data to trams that move about the rails. Trams may interlock with other cells, carry sensors or other devices, etc. Cells may be stowed in a cell stack that is deployable. Such cell-based systems may have various applications in space, on Earth, other celestial bodies, and underwater.

公开(公告)号：WO2009148625A2

公开(公告)日：2009-12-10

申请号：PCT/US2009/003444

申请日：2009-06-08

Applicant: THE SPACE ISLAND GROUP, INC. ,  MEYERS, Eugene, Walter

Inventor： MEYERS, Eugene, Walter

IPC: B64G1/40 ,  B64G1/12 ,  B64G1/22 ,  F02K9/42

CPC classification number: B64G1/002 ,  B64G1/12 ,  B64G1/402 ,  B64G1/428 ,  B64G1/44

Abstract: A launch vehicle for a space station includes a crew transport vehicle having an orbiter, a cylindrical cargo module separable from the orbiter when in low earth orbit, and a first liquid fuel rocket engine section coupled to the cargo module operable to assist in placement of the launch vehicle in low earth orbit. The first engine section is separable from the cargo module in low earth orbit. The launch vehicle also includes booster rockets operable to place the launch vehicle in low earth orbit, and a liquid fuel tank, which is convertible to form living and working spaces for the space station. The space station includes rentable space that is used to recover launch and assembly costs associated with the space station.

Abstract translation: 用于空间站的运载火箭包括具有轨道飞行器的船员运输车辆，当处于低地球轨道时与轨道运动器分离的圆柱形货物模块以及耦合到货物模块的第一液体燃料火箭发动机部分，其可操作以协助放置 运载火箭在低地球轨道。 第一个引擎部分可以与低地球轨道上的货物模块分离。 运载火箭还包括用于将运载火箭放置在低地球轨道中的增压火箭，以及可转换成空间站的生活和工作空间的液体燃料箱。 空间站包括用于恢复与空间电台有关的发射和装配成本的可租用空间。

公开(公告)号：WO2007106096A9

公开(公告)日：2007-11-08

申请号：PCT/US2006011017

申请日：2006-03-27

Applicant: SPACEHAB INC ,  JOHNSON MICHAEL D ,  BAKER JAMES D ,  EICHSTADT FRANK T ,  BAIN MICHAEL E

Inventor： JOHNSON MICHAEL D ,  BAKER JAMES D ,  EICHSTADT FRANK T ,  BAIN MICHAEL E

IPC: B64G1/12

CPC classification number: B64G1/62 ,  B64G1/12 ,  B64G1/24 ,  B64G1/646 ,  B64G2001/1092

Abstract: A modular spacecraft.

Abstract translation: 模块化航天器。

公开(公告)号：WO2023086991A2

公开(公告)日：2023-05-19

申请号：PCT/US2022/079814

申请日：2022-11-14

Applicant: ORBITAL OUTPOST X INC.

Inventor： ALONSO, Jose ,  LITVIN, Gustavo ,  NEMIROVSKY, Adolfo

IPC: B64G99/00 ,  B64G1/60 ,  B64G1/64 ,  B64G1/12 ,  B64G6/00 ,  B64G1/10 ,  B64G1/28 ,  B64G1/40

Abstract: A novel method has been proposed for implementing artificial gravity in the micro-gravity environment of space habitats (or other space environments). This will allow a number of human activities and services performed in an environment that resemble that on Earth, and additionally produce g-force of other environments (such as Moon, Mars, etc.) as required for certain experiments and/or services such as acclimating to a new g-force while in transit to another planetary body. Additionally, we presented a method and system to generate induced pseudo-gravity in selected modules leveraging magnetic elements both in wearables (6) and on selected surfaces (8, floors, seats, beds, etc.) of the module, allowing in Low Earth Orbit, normal gestures like sitting, standing-up or lying-in bed.

公开(公告)号：WO2018167161A1

公开(公告)日：2018-09-20

申请号：PCT/EP2018/056421

申请日：2018-03-14

Applicant: CENTRE NATIONAL D'ETUDES SPATIALES

Inventor： GONIDOU, Luc-Olivier

IPC: G06F17/12 ,  B64G1/12 ,  B64G1/14 ,  G06F17/50

Abstract: L'invention concerne un procédé de détermination par réanalyse d'une ambiance vibratoire d'un système couplé véhicule/passager, le véhicule étant soumis à des efforts extérieurs Fext et étant couplé à un nouveau passager comprenant x=l,..., N charge(s) utile(s), au niveau d'interfaces Ix véhicule/passager, le procédé comprenant une étape DET1) de détermination, à partir d'accélération(s) interfaciale(s) γ x_ref de référence d'un passager de référence, d'accélération(s) interfaciale(s) γ' x relatives au nouveau passager au moyen de la relation suivante (I) :

公开(公告)号：WO2004100171A3

公开(公告)日：2005-08-18

申请号：PCT/US0332748

申请日：2003-11-10

Applicant: IOSTAR CORP

Inventor： D AUSILIO ROBERT F ,  SOUTHARD BARI M ,  STUART JAMES R ,  WILLIAMS FRANK H

IPC: B64G1/10 ,  B64G1/22 ,  B64G1/40 ,  B64G1/42 ,  B64G1/50 ,  B64G1/64 ,  B64G1/66 ,  B64G1/12

CPC classification number: B64G1/408 ,  B64G1/1078 ,  B64G1/222 ,  B64G1/405 ,  B64G1/406 ,  B64G1/422 ,  B64G1/503 ,  B64G1/646 ,  B64G1/66

Abstract: An In Orbit Transportation & Recovery System (IOSTAR(TM)) (10) is disclosed. One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (19).

Abstract translation: 公开了轨道运输和恢复系统（IOSTAR（TM））（10）。 本发明的一个优选实施例包括由核反应堆（19）供电的空间拖船。

公开(公告)号：WO9819911A3

公开(公告)日：1998-07-09

申请号：PCT/US9720905

申请日：1997-11-03

Applicant: RIVERA RAMON L

Inventor： RIVERA RAMON L

IPC: B64G1/12 ,  B64G1/28 ,  B64G1/32 ,  B64G1/56 ,  B64G1/60 ,  B64G1/64 ,  B64G

CPC classification number: B64G1/646 ,  B64G1/12 ,  B64G1/28 ,  B64G1/32 ,  B64G1/60

Abstract: A space ship/space station (1) includes propulsion rockets (60) for translation and thrusters for station keeping and attitude control. The inner components (2, 8) are rotated to produce variable finite gravities, while the outer components are stationary for zero gravity. A vertical main module (2) has a horizontal network of minor modules (8) attached thereto to form the spokes and periphery of a wheel structure. This module network is rotated by electromagnetic bearings (44, 10) powered by vehicle (1) electricity. Docking nodes (68) are provided for visiting space ships. A meteor shield (84) is provided around main module (2) and the network of minor modules (8).

公开(公告)号：WO2023024311A1

公开(公告)日：2023-03-02

申请号：PCT/CN2021/135005

申请日：2021-12-02

Applicant: 鲁东大学

Inventor： 滕瑶 ,  巩庆涛 ,  孙久航 ,  李康强 ,  金丽妍 ,  何士龙 ,  王刚

IPC: B64G1/12 ,  B64G1/52 ,  B64G1/44

Abstract: 本发明公开了一种柔性太空舱，包括气动装置、太阳能发电装置和旋转装置，舱体包括第一舱体、第二舱体和第三舱体，第一舱体和第二舱体、第二舱体和第三舱体之间设有舱段连接处；第二舱体、第三舱体和舱段连接处均包括太空舱防护层；舱体内设有液压折叠件，用于辅助舱体折叠和展开；气动装置设置在舱体内部，用于对舱体进行充气和补气；本发明根据现有需求进行设计，以柔性材料为主，少了刚性材料的使用，使太空舱的重量得到了较大减轻，减少了燃料消耗，提高了飞船货舱利用率，采用高强度大分子材料复合其他材料，实现强度、密闭、保温、耐（阻）辐射等目标的同时，做到轻便、空间利用率高、可折叠等。