DE69100695T2 - Niederhaltersystem für entklappbare Elemente an einem Raumflugkörper. - Google Patents
Niederhaltersystem für entklappbare Elemente an einem Raumflugkörper.Info
- Publication number
- DE69100695T2 DE69100695T2 DE91400128T DE69100695T DE69100695T2 DE 69100695 T2 DE69100695 T2 DE 69100695T2 DE 91400128 T DE91400128 T DE 91400128T DE 69100695 T DE69100695 T DE 69100695T DE 69100695 T2 DE69100695 T2 DE 69100695T2
- Authority
- DE
- Germany
- Prior art keywords
- spacecraft
- hold
- down system
- expandable elements
- expandable
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S136/00—Batteries: thermoelectric and photoelectric
- Y10S136/291—Applications
- Y10S136/292—Space - satellite
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Aerials With Secondary Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9001352A FR2657840B1 (fr) | 1990-02-06 | 1990-02-06 | Systeme pour maintenir, en position repliee, un ensemble d'elements deployables sur un engin spatial. |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69100695D1 DE69100695D1 (de) | 1994-01-13 |
DE69100695T2 true DE69100695T2 (de) | 1994-04-14 |
Family
ID=9393423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE91400128T Expired - Fee Related DE69100695T2 (de) | 1990-02-06 | 1991-01-21 | Niederhaltersystem für entklappbare Elemente an einem Raumflugkörper. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5098042A (de) |
EP (1) | EP0441669B1 (de) |
DE (1) | DE69100695T2 (de) |
FR (1) | FR2657840B1 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5319905A (en) * | 1992-09-28 | 1994-06-14 | Spar Aerospace Limited | Panel array deployment apparatus |
US5520476A (en) * | 1993-06-18 | 1996-05-28 | Astro Aerospace Corporation | Tie-down and release mechanism for spacecraft |
US5715573A (en) * | 1995-05-22 | 1998-02-10 | Cta Space Systems, Inc. | Self latching hinge |
US5720452A (en) * | 1996-05-29 | 1998-02-24 | Lockheed Martin Corporation | Solar panel parallel mounting configuration |
US5810296A (en) * | 1996-08-29 | 1998-09-22 | Trw Inc. | Integrated restraint/release/deployment initiation device |
US6129315A (en) * | 1998-05-19 | 2000-10-10 | Hughes Electronics Corporation | Independent launch lock mechanism |
DE19913048A1 (de) * | 1999-03-23 | 2000-10-12 | Daimler Chrysler Ag | Niederhalter für Satelliten-Solargeneratoren |
AU1325801A (en) | 1999-07-16 | 2001-02-05 | Swales Aerospace | Low shock anti-friction release device |
US6311930B1 (en) | 1999-07-16 | 2001-11-06 | Swales Aerospace | Anti-friction release device |
US6119984A (en) * | 1999-07-16 | 2000-09-19 | Swales Aerospace | Low shock anti-friction release device |
FR2822803B1 (fr) * | 2001-03-29 | 2003-08-15 | Cit Alcatel | Structure de generateur solaire pour satellite comprenant des calages entre panneaux |
US6637702B1 (en) * | 2002-04-24 | 2003-10-28 | Lockheed Martin Corporation | Nested beam deployable solar array |
US7275285B1 (en) * | 2004-11-15 | 2007-10-02 | Lockheed Martin Corporation | Deployment hinge |
US8148670B2 (en) * | 2008-08-26 | 2012-04-03 | Woodward Hrt, Inc. | Rotary actuator ball-detent locking mechanism |
US8324544B2 (en) | 2010-06-02 | 2012-12-04 | Woodward Hrt, Inc. | Multi-stage fin deployment assembly |
US8624172B2 (en) | 2010-10-13 | 2014-01-07 | Woodward Hrt, Inc. | Shift lock assembly |
RU2558960C2 (ru) * | 2013-07-09 | 2015-08-10 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Держатель |
CN104590563B (zh) * | 2013-10-31 | 2016-12-07 | 北京航天长征飞行器研究所 | 一种多功能自控连接抛撒装置 |
US9605692B2 (en) | 2014-10-01 | 2017-03-28 | Woodward, Inc. | Locking rotary actuator |
RU2619497C2 (ru) * | 2015-08-13 | 2017-05-16 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Устройство удержания и освобождения раскрываемых элементов конструкции космических аппаратов |
US10562646B2 (en) * | 2016-04-21 | 2020-02-18 | Lockheed Martin Corporation | Single-point release mechanism for spacecraft |
US10351268B2 (en) | 2016-12-08 | 2019-07-16 | The Boeing Company | Systems and methods for deploying spacecraft |
CN117963165B (zh) * | 2024-04-02 | 2024-05-31 | 北京航空航天大学 | 一种基于内置螺柱展开的空间盘绕式伸展臂机构 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3267625A (en) * | 1963-05-16 | 1966-08-23 | Collins Radio Co | Latching mechanism for an extensible antenna |
US3291423A (en) * | 1965-03-15 | 1966-12-13 | Stencel Aero Eng Corp | Self-compensating power-spread parachute apparatus |
US3553984A (en) * | 1969-05-21 | 1971-01-12 | Alfred T Grumbach | Locking device |
US4151872A (en) * | 1977-12-21 | 1979-05-01 | General Dynamics Corporation | Panel deployment system |
DE2853070C3 (de) * | 1978-12-08 | 1981-10-29 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Niederhaltersystem für entfaltbare oder entklappbare Trägerelemente an Raumflugkörpern |
US4290168A (en) * | 1979-10-15 | 1981-09-22 | Rca Corporation | Hinge construction with positive locking means |
-
1990
- 1990-02-06 FR FR9001352A patent/FR2657840B1/fr not_active Expired - Fee Related
-
1991
- 1991-01-21 EP EP91400128A patent/EP0441669B1/de not_active Expired - Lifetime
- 1991-01-21 DE DE91400128T patent/DE69100695T2/de not_active Expired - Fee Related
- 1991-01-25 US US07/647,516 patent/US5098042A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2657840B1 (fr) | 1992-05-07 |
US5098042A (en) | 1992-03-24 |
EP0441669A1 (de) | 1991-08-14 |
FR2657840A1 (fr) | 1991-08-09 |
DE69100695D1 (de) | 1994-01-13 |
EP0441669B1 (de) | 1993-12-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69100695D1 (de) | Niederhaltersystem für entklappbare Elemente an einem Raumflugkörper. | |
IT1167020B (it) | Impianto di bloccaggio centralizzato per un autoveicolo | |
DE69016770T2 (de) | Abstrahlersystem für ein Raumfahrzeug. | |
NO159563C (no) | Mottaker i et globalt posisjoneringssystem. | |
DE3482991D1 (de) | Modulare unterbringung fuer rechnersystem. | |
NO155926C (no) | Transportoeranordning for et lagersystem. | |
DE3586431T2 (de) | Lokales netzwerk fuer ein numerisches datenverarbeitungssystem. | |
DE68908855T2 (de) | Steuersystem für Satellit. | |
ES295945Y (es) | Dispositivo para fijar objetos. | |
ES507232A0 (es) | Perfeccionamientos en un conjunto de carro para transporta- dores. | |
IT1143320B (it) | Sistema d antenna a schiera | |
NO166606C (no) | Antennefestesystem for bruk paa skip. | |
DE68901686T2 (de) | Strahlumkehrsystem fuer ein zweistromtriebwerk. | |
ES290201Y (es) | Un parasol para un vehiculo | |
NO160277C (no) | Posisjoneringssystem for fartoey. | |
DE68900326D1 (de) | Niederhalter-system fuer entklappbare elemente an raumflugkoerpern. | |
DK208383A (da) | Satellitkommunikationssystem for computernet | |
MX159253A (es) | Mejoras en dispositivos de autocomprobacion para un sistema de procesamiento de datos | |
ES529181A0 (es) | Un procedimiento para preparar un unguento oleoso a base de butirato-propionato de hidrocortisona | |
IT8419625A0 (it) | Sistema di fissaggio di un disco su un albero. | |
DE69109437D1 (de) | Drehgelenk für Raumfahrzeug mit einem integriertem Stapelsystem. | |
IT8322584V0 (it) | Dispositivo di ammorsamento per carichi esterni su aeroplani. | |
ES522030A0 (es) | Un metodo para preparar un poliuretano inactivado. | |
DE68904333T2 (de) | Ames-negativer diamin-haerter fuer polyurethane. | |
ES2015084B3 (es) | Metodo y aparato para montar un neumatico. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |