FR2372083A1 - - Google Patents

Info

Publication number
FR2372083A1
FR2372083A1 FR7735757A FR7735757A FR2372083A1 FR 2372083 A1 FR2372083 A1 FR 2372083A1 FR 7735757 A FR7735757 A FR 7735757A FR 7735757 A FR7735757 A FR 7735757A FR 2372083 A1 FR2372083 A1 FR 2372083A1
Authority
FR
France
Prior art keywords
support
fixed
central
link
link member
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
Application number
FR7735757A
Other languages
French (fr)
Other versions
FR2372083B1 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Leonardo SpA
Original Assignee
Aeritalia SpA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from IT6984676 external-priority
Application filed by Aeritalia SpA filed Critical Aeritalia SpA
Publication of FR2372083A1 publication Critical patent/FR2372083A1/fr
Application granted granted Critical
Publication of FR2372083B1 publication Critical patent/FR2372083B1/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles

Abstract

Structure porteuse pour un satellite artificiel. Structure porteuse pour un satellite artificiel qui comprend un élément de liaison pour relier celle-ci à un véhicule de lancement, une structure de liaison centrale rigide fixée à l'élément de liaison et s'étendant le long de l'axe de la structure porteuse, deux plates-formes de support planes, fixées de part et d'autre de la structure de liaison centrale, cette dernière et les parties correspondantes de deux plates-formes de support formant un polygone, une troisième plate-forme de support plane étant fixée à l'extrémité de la structure de liaison centrale. Concerne des perfectionnements aux satellites artificiels de télécommunications, d'observation, météorologiques et autres.Support structure for an artificial satellite. Support structure for an artificial satellite which comprises a link member for connecting it to a launch vehicle, a rigid central link structure attached to the link member and extending along the axis of the carrier structure , two flat support platforms, fixed on either side of the central connecting structure, the latter and the corresponding parts of two support platforms forming a polygon, a third flat support platform being fixed at the end of the central link structure. Concerns improvements to artificial telecommunications, observation, meteorological and other satellites.

FR7735757A 1976-11-29 1977-11-28 Expired FR2372083B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT6984676 1976-11-29

Publications (2)

Publication Number Publication Date
FR2372083A1 true FR2372083A1 (en) 1978-06-23
FR2372083B1 FR2372083B1 (en) 1982-10-29

Family

ID=11312954

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7735757A Expired FR2372083B1 (en) 1976-11-29 1977-11-28

Country Status (3)

Country Link
DE (1) DE2753188A1 (en)
FR (1) FR2372083B1 (en)
GB (1) GB1557500A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2579954A1 (en) * 1985-04-08 1986-10-10 Rca Corp
EP0238840A2 (en) * 1986-03-22 1987-09-30 ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung Payload transport and operating system for space vehicles
FR2695906A1 (en) * 1992-09-21 1994-03-25 Gen Electric Spaceship-launcher association and transition piece for this association.
EP0823374A2 (en) * 1996-08-05 1998-02-11 The Boeing Company One piece spacecraft frame
EP0849168A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module
WO2011135230A1 (en) 2010-04-28 2011-11-03 Astrium Sas Satellite having a simplified, streamlined, and economical structure, and method for implementing same
CN102616385A (en) * 2012-04-11 2012-08-01 深圳航天东方红海特卫星有限公司 Truss-type satellite structure with central capsule

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4575029A (en) * 1979-10-30 1986-03-11 Trw Inc. Spacecraft for use in conjunction with a reusable space shuttle
US4943014A (en) * 1979-10-30 1990-07-24 Trw Inc. Soft ride method for changing the altitude or position of a spacecraft in orbit
DE3002551A1 (en) * 1980-01-25 1981-07-30 Peter 1000 Berlin Rohr Interplanetary spacecraft transporter unit - can carry several craft to deployment region in space without using their fuel, is rocket-propelled, steered, braked
GB8526723D0 (en) * 1985-10-30 1985-12-04 Rca Corp Spacecraft structure
US4854526A (en) * 1987-08-10 1989-08-08 Hughes Aircraft Company Spacecraft design enabling the compact nesting of multiple spacecraft in the launch vehicle
US5314146A (en) * 1992-03-13 1994-05-24 Spectrum Astro, Inc. Multi-mission spacecraft bus having space frame structural design
US5803402A (en) * 1994-04-11 1998-09-08 Composite Optics, Inc. System and method for the construction of spacecraft structures
US5950965A (en) * 1997-07-17 1999-09-14 Lockheed Martin Corporation Split shell spacecraft
CN102372092A (en) * 2010-08-17 2012-03-14 上海卫星工程研究所 Configuration for low-earth-orbit remote sensing satellite and mounting method thereof
CN103192998B (en) * 2013-01-30 2015-07-08 航天东方红卫星有限公司 System-level emergency response device of spacecraft
US9296493B2 (en) * 2013-02-28 2016-03-29 The Boeing Company Spacecraft with open sides

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258225A (en) * 1964-03-13 1966-06-28 Fred H Esch Satellite mounting structure
FR2309403A1 (en) * 1974-12-23 1976-11-26 Rca Corp SPATIALSHIP

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258225A (en) * 1964-03-13 1966-06-28 Fred H Esch Satellite mounting structure
FR2309403A1 (en) * 1974-12-23 1976-11-26 Rca Corp SPATIALSHIP

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/68 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2579954A1 (en) * 1985-04-08 1986-10-10 Rca Corp
EP0238840A2 (en) * 1986-03-22 1987-09-30 ERNO Raumfahrttechnik Gesellschaft mit beschränkter Haftung Payload transport and operating system for space vehicles
JPS62227898A (en) * 1986-03-22 1987-10-06 Erno Raumfahrttechnik Gmbh Driving device combining load transport for space craft
EP0238840A3 (en) * 1986-03-22 1989-09-06 Erno Raumfahrttechnik Gesellschaft Mit Beschrankter Haftung Payload transport and operating system for space vehicles
FR2695906A1 (en) * 1992-09-21 1994-03-25 Gen Electric Spaceship-launcher association and transition piece for this association.
EP0823374A3 (en) * 1996-08-05 1998-11-18 The Boeing Company One piece spacecraft frame
EP0823374A2 (en) * 1996-08-05 1998-02-11 The Boeing Company One piece spacecraft frame
EP0849168A1 (en) * 1996-12-20 1998-06-24 TRW Inc. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module
WO2011135230A1 (en) 2010-04-28 2011-11-03 Astrium Sas Satellite having a simplified, streamlined, and economical structure, and method for implementing same
FR2959490A1 (en) * 2010-04-28 2011-11-04 Astrium Sas SATELLITE HAVING A SIMPLIFIED, ALLEGE AND ECONOMIC STRUCTURE AND ITS IMPLEMENTING METHOD
US9446863B2 (en) 2010-04-28 2016-09-20 Airbus Defence And Space Sas Satellite having a simplified, streamlined, and economical structure, and method for implementing same
CN102616385A (en) * 2012-04-11 2012-08-01 深圳航天东方红海特卫星有限公司 Truss-type satellite structure with central capsule
CN102616385B (en) * 2012-04-11 2015-01-14 深圳航天东方红海特卫星有限公司 Truss-type satellite structure with central capsule

Also Published As

Publication number Publication date
DE2753188A1 (en) 1978-06-01
GB1557500A (en) 1979-12-12
FR2372083B1 (en) 1982-10-29

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Legal Events

Date Code Title Description
ST Notification of lapse