ES2120338A1 - Sistema de fijacion y separacion para satelites. - Google Patents

Sistema de fijacion y separacion para satelites.

Info

Publication number
ES2120338A1
ES2120338A1 ES09501994A ES9501994A ES2120338A1 ES 2120338 A1 ES2120338 A1 ES 2120338A1 ES 09501994 A ES09501994 A ES 09501994A ES 9501994 A ES9501994 A ES 9501994A ES 2120338 A1 ES2120338 A1 ES 2120338A1
Authority
ES
Spain
Prior art keywords
fixing
satellite
metal
satellites
separation system
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
ES09501994A
Other languages
English (en)
Other versions
ES2120338B1 (es
Inventor
Miguel Canay
Venancio Uribarri
Fernando Cespedosa
Jorge Avila
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.)
Airbus Defence and Space SA
Original Assignee
Construcciones Aeronauticas CASA SA
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
Application filed by Construcciones Aeronauticas CASA SA filed Critical Construcciones Aeronauticas CASA SA
Priority to ES09501994A priority Critical patent/ES2120338B1/es
Priority to EP96500010A priority patent/EP0768241A1/en
Publication of ES2120338A1 publication Critical patent/ES2120338A1/es
Application granted granted Critical
Publication of ES2120338B1 publication Critical patent/ES2120338B1/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64G1/64—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)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Clamps And Clips (AREA)

Abstract

SISTEMA DE FIJACION Y SEPARACION PARA SATELITES. COMPRENDE UNA PIEZA (1) DE FIJACION QUE SE ATORNILLA AL ARO SUPERIOR (2) DEL ADAPTADOR (3) DEL COHETE LANZADOR, UNA BANDA TENSORA (6) CONSISTENTE EN UN FLEJE METALICO EN DOS TROZOS, UNAS PIEZAS METALICAS CURVAS (7) DE FIJACION DEL SATELITE (8) QUE TIENEN UN CUERPO CILINDRICO DE PARED DELGADA CON EJE DE GIRO METALICO (9) EN SU PARTE INFERIOR FORMADO POR VARIAS OREJERAS Y QUE SE APOYAN CON SU PARTE SUPERIOR EN EL ARO INFERIOR (10) DEL SATELITE (8), RODEANDOLO Y APRETANDOLO, Y UNAS LEVAS DE APRIETE (5) QUE TIENEN CADA UNA DOS EJES DE GIRO (9, 4), UNO (9) COINCIDENTE CON EL DE DICHAS PIEZAS METALICAS (7) Y EL OTRO (4) COMPARTIDO CON DICHA PIEZA (1). LA INVENCION SIMPLIFICA LA SUJECION DEL SATELITE AL COHETE LANZADOR Y SU SUELTA AL ENTRAR EN ORBITA. FIGURA 2.
ES09501994A 1995-10-16 1995-10-16 Sistema de fijacion y separacion para satelites. Expired - Lifetime ES2120338B1 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES09501994A ES2120338B1 (es) 1995-10-16 1995-10-16 Sistema de fijacion y separacion para satelites.
EP96500010A EP0768241A1 (en) 1995-10-16 1996-01-31 Fastening and separating system for satellites

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES09501994A ES2120338B1 (es) 1995-10-16 1995-10-16 Sistema de fijacion y separacion para satelites.

Publications (2)

Publication Number Publication Date
ES2120338A1 true ES2120338A1 (es) 1998-10-16
ES2120338B1 ES2120338B1 (es) 1999-05-01

Family

ID=8291850

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09501994A Expired - Lifetime ES2120338B1 (es) 1995-10-16 1995-10-16 Sistema de fijacion y separacion para satelites.

Country Status (2)

Country Link
EP (1) EP0768241A1 (es)
ES (1) ES2120338B1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1002717A2 (en) 1998-11-18 2000-05-24 Construcciones Aeronauticas, S.A. A system for the modification of the rigidity/damping properties of structural joints

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2131476B1 (es) 1997-09-26 2000-03-01 Const Aeronauticas Sa Sistema de fijacion y separacion de satelites.
CN103754391B (zh) * 2014-01-02 2016-05-04 上海宇航系统工程研究所 大型空间机构压紧释放装置
CA2968300C (en) 2014-11-25 2021-06-29 Airbus Defence And Space, S.A. Separation system for separable elements of spacecrafts and launchers
CA3047680C (en) 2016-12-22 2024-01-02 Airbus Defence and Space S.A. Connection/separation device to separate satellites from launchers or from satellite dispensers
CN107860274B (zh) * 2017-11-23 2019-09-06 北京宇航系统工程研究所 一种挂钩式连接与解锁装置
CN110925277B (zh) * 2019-11-13 2021-03-09 北京机械设备研究所 一种基于摇臂连杆的分离装置及机械分离系统
CN111717420B (zh) * 2020-07-21 2023-08-22 哈尔滨工业大学 压紧机构精准限位展开装置及展开限位方法
CN114018104B (zh) * 2021-09-24 2023-09-26 广州冕巢航天科技有限公司 一种分离装置
EP4588811A1 (en) 2024-01-16 2025-07-23 Aciturri Engineering, S.L. System for fixing and separating structures
EP4714834A1 (de) * 2024-09-20 2026-03-25 EXOLAUNCH GmbH Vorrichtung zum lösbaren befestigen von nutzlast an einem raumfahrzeug

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3111900A (en) * 1961-03-30 1963-11-26 United Aircraft Corp Missile interstage separating device
US3429477A (en) * 1967-05-17 1969-02-25 Webb James E Apparatus for ejection of an instrument cover
US3737117A (en) * 1971-07-06 1973-06-05 Nasa Docking structure for spacecraft
US3753536A (en) * 1970-10-02 1973-08-21 British Aircraft Corp Ltd Space vehicle coupling mechanisms
EP0081401A1 (fr) * 1981-11-26 1983-06-15 AEROSPATIALE Société Nationale Industrielle Système permettant le maintien temporaire et la libération de deux parties, plus particulièrement dans le domaine spatial
US5197695A (en) * 1991-03-04 1993-03-30 Saab Space Aktiebolag Locking device for a band or the like, subject to a tensile force

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3346929A (en) * 1966-03-04 1967-10-17 James E Webb Latching mechanism
US3564564A (en) * 1969-11-21 1971-02-16 Nasa Latching mechanism
FR2670844B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Mecanisme de mise en tension, liberable a distance, d'un organe souple tel qu'une sangle et dispositif de raccordement rigide de deux ensembles mecaniques au moyen d'un tel mecanisme.

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3111900A (en) * 1961-03-30 1963-11-26 United Aircraft Corp Missile interstage separating device
US3429477A (en) * 1967-05-17 1969-02-25 Webb James E Apparatus for ejection of an instrument cover
US3753536A (en) * 1970-10-02 1973-08-21 British Aircraft Corp Ltd Space vehicle coupling mechanisms
US3737117A (en) * 1971-07-06 1973-06-05 Nasa Docking structure for spacecraft
EP0081401A1 (fr) * 1981-11-26 1983-06-15 AEROSPATIALE Société Nationale Industrielle Système permettant le maintien temporaire et la libération de deux parties, plus particulièrement dans le domaine spatial
US5197695A (en) * 1991-03-04 1993-03-30 Saab Space Aktiebolag Locking device for a band or the like, subject to a tensile force

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1002717A2 (en) 1998-11-18 2000-05-24 Construcciones Aeronauticas, S.A. A system for the modification of the rigidity/damping properties of structural joints
EP1002717A3 (en) * 1998-11-18 2000-10-11 Construcciones Aeronauticas, S.A. A system for the modification of the rigidity/damping properties of structural joints
US6305871B1 (en) 1998-11-18 2001-10-23 Construcciones Aeronauticas, S.A. System for the modification of the rigidity and damping properties of structural joints

Also Published As

Publication number Publication date
EP0768241A1 (en) 1997-04-16
ES2120338B1 (es) 1999-05-01

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