FR2421799A1 - Structure pour les satellites - Google Patents
Structure pour les satellitesInfo
- Publication number
- FR2421799A1 FR2421799A1 FR7907728A FR7907728A FR2421799A1 FR 2421799 A1 FR2421799 A1 FR 2421799A1 FR 7907728 A FR7907728 A FR 7907728A FR 7907728 A FR7907728 A FR 7907728A FR 2421799 A1 FR2421799 A1 FR 2421799A1
- Authority
- FR
- France
- Prior art keywords
- central
- satellites
- modules
- section
- satellite
- 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.)
- Granted
Links
- 230000007704 transition 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
- B64G1/223—Modular spacecraft systems
-
- 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
- B64G1/642—Clamps, e.g. Marman clamps
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Details Of Aerials (AREA)
- Radio Relay Systems (AREA)
- Reinforcement Elements For Buildings (AREA)
Abstract
L'invention vise une structure pour satellites. Cette structure comporte une structure centrale en treillis 1 fait d'une matière thermostable dont chaque noeud 3, 31 , 32 , 33 , 34 , 35 , 36 , 37 présente un point de support 4, 41 , 4 2 , 43 , 44 , 45 , 46 , 47 permettant le raccordement statiquement déterminé de modules 6, 7, 8, 9, 10, 11 à l'aide de boulons ou vis ou bien de colliers de serrage. Cette structure centrale 1 est pourvue d'un adapteur intermédiaire assurant la transition d'une section circulaire à une quelconque autre section. Une telle structure permet l'assemblage d'un satellite comprenant une combinaison arbitraire de différents modules sur la même structure centrale.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2815216A DE2815216C2 (de) | 1978-04-08 | 1978-04-08 | Satellitenstruktur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2421799A1 true FR2421799A1 (fr) | 1979-11-02 |
FR2421799B1 FR2421799B1 (fr) | 1983-05-27 |
Family
ID=6036456
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7907728A Granted FR2421799A1 (fr) | 1978-04-08 | 1979-03-22 | Structure pour les satellites |
Country Status (5)
Country | Link |
---|---|
CH (1) | CH642922A5 (fr) |
DE (1) | DE2815216C2 (fr) |
FR (1) | FR2421799A1 (fr) |
GB (1) | GB2018211B (fr) |
IT (1) | IT7967734A0 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4834325A (en) * | 1985-03-20 | 1989-05-30 | Space Industries, Inc. | Modular spacecraft system |
GB8526723D0 (en) * | 1985-10-30 | 1985-12-04 | Rca Corp | Spacecraft structure |
DE3609770A1 (de) * | 1986-03-22 | 1987-10-01 | Erno Raumfahrttechnik Gmbh | Nutzlasttransport- und -betriebseinrichtung fuer raumfahrzeuge |
US5337980A (en) * | 1992-09-21 | 1994-08-16 | General Electric Co. | Spacecraft-to-launch-vehicle transition |
US5961076A (en) * | 1996-12-20 | 1999-10-05 | Trw Inc. | Modular spacecraft development process |
US5931418A (en) * | 1996-12-20 | 1999-08-03 | Trw Inc. | Functionally independent spacecraft module |
US5904317A (en) * | 1996-12-20 | 1999-05-18 | Trw Inc. | Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module |
US5897080A (en) * | 1996-12-20 | 1999-04-27 | Trw Inc. | Externally mountable spacecraft equipment module |
EP0849166A1 (fr) * | 1996-12-20 | 1998-06-24 | TRW Inc. | Architecture modulaire dans un engin spatial. |
CN112298605B (zh) * | 2020-09-29 | 2022-03-04 | 北京空间飞行器总体设计部 | 一种板杆式卫星主结构 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2835548A (en) * | 1957-08-01 | 1958-05-20 | Robert C Baumann | Satellite structure |
US3258225A (en) * | 1964-03-13 | 1966-06-28 | Fred H Esch | Satellite mounting structure |
GB1169342A (en) * | 1966-01-17 | 1969-11-05 | British Aircraft Corp Ltd Form | Improvements in Rocket Powered Aerial and Space Vehicles |
-
1978
- 1978-04-08 DE DE2815216A patent/DE2815216C2/de not_active Expired
-
1979
- 1979-02-14 GB GB7905167A patent/GB2018211B/en not_active Expired
- 1979-03-06 CH CH218779A patent/CH642922A5/de not_active IP Right Cessation
- 1979-03-22 FR FR7907728A patent/FR2421799A1/fr active Granted
- 1979-04-06 IT IT7967734A patent/IT7967734A0/it unknown
Non-Patent Citations (1)
Title |
---|
EXBK/78 * |
Also Published As
Publication number | Publication date |
---|---|
CH642922A5 (de) | 1984-05-15 |
FR2421799B1 (fr) | 1983-05-27 |
GB2018211A (en) | 1979-10-17 |
DE2815216C2 (de) | 1984-04-26 |
GB2018211B (en) | 1982-06-03 |
DE2815216A1 (de) | 1979-10-11 |
IT7967734A0 (it) | 1979-04-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |