ES2140499T3 - Procedimiento de fabricacion de una estructura de soporte para un vehiculo espacial y estructura de soporte. - Google Patents
Procedimiento de fabricacion de una estructura de soporte para un vehiculo espacial y estructura de soporte.Info
- Publication number
- ES2140499T3 ES2140499T3 ES94202695T ES94202695T ES2140499T3 ES 2140499 T3 ES2140499 T3 ES 2140499T3 ES 94202695 T ES94202695 T ES 94202695T ES 94202695 T ES94202695 T ES 94202695T ES 2140499 T3 ES2140499 T3 ES 2140499T3
- Authority
- ES
- Spain
- Prior art keywords
- support structure
- manufacturing procedure
- space vehicle
- chuck
- support
- 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
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 230000008030 elimination Effects 0.000 abstract 1
- 238000003379 elimination reaction Methods 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 238000004804 winding Methods 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
-
- 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
- B64G1/223—Modular spacecraft systems
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Moulding By Coating Moulds (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
UN METODO PARA FABRICAR UNA ESTRUCTURA DE SOPORTE (1,2) DE UNA NAVE ESPACIAL, QUE TIENE UNA PARTE INFERIOR FORMADA ADAPTADA PARA AJUSTAR EN LA PARTE SUPERIOR DE UN LANZADOR, COMPRENDE LOS PASOS DE PROPORCIONAR UN MANDRIL QUE TENGA LA FORMA APROPIADA PARA LA ESTRUCTURA DE SOPORTE (1,2), MATERIAL DE FILAMENTO DE BOBINADO EN EL MANDRIL, MATERIAL DE FILAMENTO DE FIJACION MEDIANTE LA APLICACION DE UN MATERIAL DE MATRIZ, Y ELIMINACION DE LA ESTRUCTURA DE SOPORTE (1,2) FORMADA ASI DESDE EL MANDRIL.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP94202695A EP0703144B1 (en) | 1994-09-20 | 1994-09-20 | Method for manufacturing a bearing structure for a spacecraft, and bearing structure |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2140499T3 true ES2140499T3 (es) | 2000-03-01 |
Family
ID=8217207
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES94202695T Expired - Lifetime ES2140499T3 (es) | 1994-09-20 | 1994-09-20 | Procedimiento de fabricacion de una estructura de soporte para un vehiculo espacial y estructura de soporte. |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0703144B1 (es) |
DE (1) | DE69422621T2 (es) |
ES (1) | ES2140499T3 (es) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5848767A (en) * | 1996-08-05 | 1998-12-15 | The Boeing Company | One piece spacecraft frame |
US9205625B2 (en) * | 2013-02-19 | 2015-12-08 | The Boeing Company | Spiral laminated structural cone and manufacturing method |
DE102022114410A1 (de) * | 2022-06-08 | 2023-12-14 | Mt Aerospace Ag | Zentralrohr für Satelliten und Raumfahrzeuge |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3960626A (en) * | 1971-01-08 | 1976-06-01 | Martin Marietta Corporation | Method of making high performance ablative tape |
US3700535A (en) * | 1971-03-12 | 1972-10-24 | Atomic Energy Commission | Carbon fiber structure and method of forming same |
DE2518644C3 (de) * | 1975-04-26 | 1978-03-30 | Dornier System Gmbh, 7990 Friedrichshafen | Verfahren zum Herstellen einer Kegelschale und Kegelschale |
US4682744A (en) * | 1985-04-08 | 1987-07-28 | Rca Corporation | Spacecraft structure |
US4851065A (en) * | 1986-01-17 | 1989-07-25 | Tyee Aircraft, Inc. | Construction of hollow, continuously wound filament load-bearing structure |
-
1994
- 1994-09-20 ES ES94202695T patent/ES2140499T3/es not_active Expired - Lifetime
- 1994-09-20 EP EP94202695A patent/EP0703144B1/en not_active Expired - Lifetime
- 1994-09-20 DE DE69422621T patent/DE69422621T2/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE69422621T2 (de) | 2000-08-31 |
EP0703144B1 (en) | 2000-01-12 |
EP0703144A1 (en) | 1996-03-27 |
DE69422621D1 (de) | 2000-02-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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