FR2736616B1 - Deverrouilleur a ecrou fendu pour ejecteur de microsatellite - Google Patents

Deverrouilleur a ecrou fendu pour ejecteur de microsatellite

Info

Publication number
FR2736616B1
FR2736616B1 FR9508503A FR9508503A FR2736616B1 FR 2736616 B1 FR2736616 B1 FR 2736616B1 FR 9508503 A FR9508503 A FR 9508503A FR 9508503 A FR9508503 A FR 9508503A FR 2736616 B1 FR2736616 B1 FR 2736616B1
Authority
FR
France
Prior art keywords
releaser
microsatellite
ejector
slotted nut
slotted
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
Application number
FR9508503A
Other languages
English (en)
Other versions
FR2736616A1 (fr
Inventor
Jean Pierre Aubret
Michel Barriere
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR9508503A priority Critical patent/FR2736616B1/fr
Priority to US08/677,316 priority patent/US5755407A/en
Publication of FR2736616A1 publication Critical patent/FR2736616A1/fr
Application granted granted Critical
Publication of FR2736616B1 publication Critical patent/FR2736616B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641Interstage or payload connectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators
    • B64G1/6455Pyrotechnics; Using heat

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Damping Devices (AREA)
  • Portable Nailing Machines And Staplers (AREA)
FR9508503A 1995-07-13 1995-07-13 Deverrouilleur a ecrou fendu pour ejecteur de microsatellite Expired - Lifetime FR2736616B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9508503A FR2736616B1 (fr) 1995-07-13 1995-07-13 Deverrouilleur a ecrou fendu pour ejecteur de microsatellite
US08/677,316 US5755407A (en) 1995-07-13 1996-07-02 Slotted nut type releasing device for microsatellite ejector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9508503A FR2736616B1 (fr) 1995-07-13 1995-07-13 Deverrouilleur a ecrou fendu pour ejecteur de microsatellite

Publications (2)

Publication Number Publication Date
FR2736616A1 FR2736616A1 (fr) 1997-01-17
FR2736616B1 true FR2736616B1 (fr) 1997-09-19

Family

ID=9480972

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9508503A Expired - Lifetime FR2736616B1 (fr) 1995-07-13 1995-07-13 Deverrouilleur a ecrou fendu pour ejecteur de microsatellite

Country Status (2)

Country Link
US (1) US5755407A (fr)
FR (1) FR2736616B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106742081A (zh) * 2016-11-29 2017-05-31 航天东方红卫星有限公司 一种基于旋转压环解锁的分离机构

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6129315A (en) * 1998-05-19 2000-10-10 Hughes Electronics Corporation Independent launch lock mechanism
US6138951A (en) * 1998-08-10 2000-10-31 Mcdonnell Douglas Corporation Spacecraft dispensing system
GR1003755B (el) * 2000-03-31 2002-01-15 Αεροσκαφος με αποχωριζομενη καμπινα διαφυγης επιβατων εξοπλισμενη με αλεξιπτωτα-αεροσακκους-καθισματα απορροφησης κρουσεως και συμβατικο αεροσκαφος εξοπλισμενο με τα συστηματα αυτα ασφαλειας
US6450454B1 (en) * 2000-12-29 2002-09-17 Space Systems/Loral, Inc. Spacecraft attack and distress ejectable recorder
US6948686B2 (en) * 2002-04-10 2005-09-27 Walter Holemans Constant rate deployment device
US6679154B1 (en) * 2002-11-25 2004-01-20 Lockheed Martin Corporation Passive dynamically disconnecting arm
US20060097113A1 (en) * 2004-10-18 2006-05-11 Aai Corporation Payload ejection system
US7644891B2 (en) * 2007-05-25 2010-01-12 The Boeing Company Spacecraft low tumble linear release system
US8052092B2 (en) * 2009-01-30 2011-11-08 The Boeing Company Method and apparatus for satellite orbital change using space debris
US20110060498A1 (en) * 2009-07-10 2011-03-10 Cannon John L Data recovery apparatus and system
US8939409B2 (en) 2012-05-07 2015-01-27 The Johns Hopkins University Adaptor system for deploying small satellites
US11066192B2 (en) 2017-08-04 2021-07-20 Rocket Lab Usa, Inc. Satellite deployer door with clutch bearing
KR102002306B1 (ko) * 2018-01-08 2019-07-22 주식회사 버츄얼랩 큐브위성 우주 분리장치
US10730625B1 (en) * 2019-02-11 2020-08-04 Raytheon Company Payload ejector with shock attenuation device

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3174706A (en) * 1960-12-08 1965-03-23 Hermann R Wagner Separation device
US3547375A (en) * 1968-03-22 1970-12-15 Trw Inc Passive release mechanism for space vehicles
US4067308A (en) * 1976-11-02 1978-01-10 The United States Of America As Represented By The United States Department Of Energy Spin ejector
US4625619A (en) * 1984-07-02 1986-12-02 The United States Of America As Represented By The Secretary Of The Navy Device for separation and launch of a body with linear and rotational velocity
US4632339A (en) * 1984-12-24 1986-12-30 Hughes Aircraft Company Spacecraft payload ejection mechanism
FR2616856B1 (fr) * 1987-06-16 1991-12-13 Aerospatiale Mecanisme de commande d'ecartement rapide et controle de deux pieces en contact
FR2637252B1 (fr) * 1988-10-05 1990-12-28 Aerospatiale Dispositif de solidarisation/desolidarisation provisoire de deux elements l'un a l'autre, et de separation ulterieure
FR2661466B1 (fr) * 1990-04-25 1992-08-07 Aerospatiale Soc Nat Industrielle Mecanisme de liaison a deverrouillage rapide, utilisable notamment sur des engins spatiaux.
FR2697871B1 (fr) * 1992-11-09 1995-02-24 Aerospatiale Dispositif de maintien puis d'écartement, selon une séquence contrôlée, d'un objet par rapport à un support.
FR2713326B1 (fr) * 1993-12-06 1996-01-26 Aerospatiale Dispositif pour éjecter, par voie pneumatique, un objet par rapport à une structure.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106742081A (zh) * 2016-11-29 2017-05-31 航天东方红卫星有限公司 一种基于旋转压环解锁的分离机构

Also Published As

Publication number Publication date
US5755407A (en) 1998-05-26
FR2736616A1 (fr) 1997-01-17

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Legal Events

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TP Transmission of property
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