ES2115192T3 - Adaptador estructural para el compartimento de carga de un cohete transportador. - Google Patents
Adaptador estructural para el compartimento de carga de un cohete transportador.Info
- Publication number
- ES2115192T3 ES2115192T3 ES94830029T ES94830029T ES2115192T3 ES 2115192 T3 ES2115192 T3 ES 2115192T3 ES 94830029 T ES94830029 T ES 94830029T ES 94830029 T ES94830029 T ES 94830029T ES 2115192 T3 ES2115192 T3 ES 2115192T3
- Authority
- ES
- Spain
- Prior art keywords
- adapter
- equipment
- missions
- satellite
- satellites
- 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 - Lifetime
Links
- 230000005611 electricity Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- 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
- B64G1/641—Interstage or payload connectors
-
- 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
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/242—Orbits and trajectories
- B64G1/2427—Transfer orbits
-
- 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
- B64G1/641—Interstage or payload connectors
- B64G1/643—Interstage or payload connectors for arranging multiple satellites in a single launcher
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1085—Swarms and constellations
Abstract
UN ADAPTADOR ESTRUCTURAL PARA EL EMPLAZAMIENTO DE CARGA DE UN MISIL PORTADOR (2) ADAPTADO PARA LANZAR UN PAR DE SATELITES (22,24) COMPRENDE UN CUERPO CILINDRICO HUECO (18) QUE TIENE UN PRIMER EXTREMO (20) DE CONEXION LIBERABLE A UN SATELITE PRINCIPAL (22) Y UN SEGUNDO EXTREMO OPUESTO (21) DE CONEXION LIBERABLE A UNA PLATAFORMA DE SERVICIO (16). UN SATELITE SECUNDARIO (24) PUEDE ESTAR LOCALIZADO DENTRO DEL CUERPO HUECO (18). DICHO CUERPO (18) SOSTIENE UN EQUIPO SOBRE TABLERO (33) QUE INCLUYE UNOS ELEMENTOS GENERADORES ELECTRICOS (28,32A), UNOS ELEMENTOS PARA ALMACENAR ENERGIA ELECTRICA Y MIEMBROS PARA SUMINISTRAR LA ELECTRICIDAD AL EQUIPO ASOCIADO CON EL CUERPO (24;33). EL ADAPTADOR (18) SUJETA EL EQUIPO PARA PROCESAR Y MANEJAR DATOS, CONTROLANDO LA TEMPERATURA DEL EQUIPO INTERNO, CONTROLANDO LA ALTITUD DEL PROPIO ADAPTADOR, TRANSMITIENDO DATOS A TIERRA Y RECIBIENDO DATOS Y MANDOS DESDE LA TIERRA. TODO ESTO POSIBILITA QUE EL ADAPTADOR (18) LLEVE A CABO MISIONES PROGRAMADAS COMO UN SATELITE.EL ADAPTADOR (18) PUEDE ASISTIR A UNO DE LOS SATELITES (22,24) DURANTE EL CUMPLIMIENTO DE AL MENOS PARTE DE SU O SUS MISIONES Y/O PUEDE LLEVAR A CABO MISIONES ESPACIALES INDEPENDIENTES.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP94830029A EP0665162B1 (en) | 1994-01-28 | 1994-01-28 | Structural adaptor for the loading bay of a carrier rocket |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2115192T3 true ES2115192T3 (es) | 1998-06-16 |
Family
ID=8218369
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES94830029T Expired - Lifetime ES2115192T3 (es) | 1994-01-28 | 1994-01-28 | Adaptador estructural para el compartimento de carga de un cohete transportador. |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0665162B1 (es) |
AT (1) | ATE164814T1 (es) |
DE (1) | DE69409493T2 (es) |
ES (1) | ES2115192T3 (es) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT2361U1 (de) * | 1997-08-13 | 1998-09-25 | Blau Automobiltechnik Gmbh | Vorrichtung zum galvanisieren von schöpfenden teilen |
SE515850C2 (sv) | 2000-09-18 | 2001-10-15 | Saab Ericsson Space Ab | Anordning och metod vid en rymdfarkost |
NL1020271C2 (nl) * | 2002-03-28 | 2003-09-30 | Dutch Space B V | Ruimtevaartuig en werkwijze voor het samenstellen van een dergelijk ruimtevaartuig, alsmede adaptor te gebruiken in een dergelijk ruimtevaartuig. |
FR2980177B1 (fr) * | 2011-09-20 | 2014-07-11 | Centre Nat Etd Spatiales | Baie propulsive |
FR3002594B1 (fr) | 2013-02-26 | 2016-09-30 | Snecma | Module de propulsion spatiale a propulsion electrique et chimique a propergol solide |
CN103963997A (zh) * | 2014-05-06 | 2014-08-06 | 上海卫星工程研究所 | 一种小型卫星多边形承力筒 |
CN104648693B (zh) * | 2014-12-23 | 2017-01-11 | 中国科学院长春光学精密机械与物理研究所 | 用于平台载荷一体化的卫星结构 |
DE102017126609A1 (de) * | 2017-11-13 | 2019-05-16 | Arianegroup Gmbh | Trägerrakete mit Solarzellen, Herstellungsverfahren und Transportverfahren |
CN113148241B (zh) * | 2021-04-28 | 2023-08-11 | 北京星途探索科技有限公司 | 一种串联式载荷适配器 |
CN115743602A (zh) * | 2022-09-28 | 2023-03-07 | 北京微纳星空科技有限公司 | 卫星平台 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4664343A (en) * | 1984-08-29 | 1987-05-12 | Scott Science & Technology, Inc. | Satelite transfer vehicle |
FR2649667B1 (fr) * | 1989-07-17 | 1991-09-20 | Centre Nat Etd Spatiales | Procede de lancement dans l'espace d'une capsule et moyen de lancement correspondant |
-
1994
- 1994-01-28 ES ES94830029T patent/ES2115192T3/es not_active Expired - Lifetime
- 1994-01-28 EP EP94830029A patent/EP0665162B1/en not_active Expired - Lifetime
- 1994-01-28 AT AT94830029T patent/ATE164814T1/de not_active IP Right Cessation
- 1994-01-28 DE DE69409493T patent/DE69409493T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69409493D1 (de) | 1998-05-14 |
ATE164814T1 (de) | 1998-04-15 |
EP0665162A1 (en) | 1995-08-02 |
EP0665162B1 (en) | 1998-04-08 |
DE69409493T2 (de) | 1998-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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