FR3109928B1 - Dispositif de déploiement amélioré pour nano-satellite - Google Patents

Dispositif de déploiement amélioré pour nano-satellite Download PDF

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Publication number
FR3109928B1
FR3109928B1 FR2004623A FR2004623A FR3109928B1 FR 3109928 B1 FR3109928 B1 FR 3109928B1 FR 2004623 A FR2004623 A FR 2004623A FR 2004623 A FR2004623 A FR 2004623A FR 3109928 B1 FR3109928 B1 FR 3109928B1
Authority
FR
France
Prior art keywords
clamping element
deployment device
satellite
support frame
nano
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.)
Active
Application number
FR2004623A
Other languages
English (en)
Other versions
FR3109928A1 (fr
Inventor
Olivier Deslandes
Jacques Sicre
Lionel Bonnes
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.)
Mecano I D
Centre National dEtudes Spatiales CNES
Original Assignee
Mecano I D
Centre National dEtudes Spatiales CNES
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 Mecano I D, Centre National dEtudes Spatiales CNES filed Critical Mecano I D
Priority to FR2004623A priority Critical patent/FR3109928B1/fr
Priority to EP21731253.7A priority patent/EP4149841A1/fr
Priority to PCT/FR2021/050818 priority patent/WO2021229178A1/fr
Publication of FR3109928A1 publication Critical patent/FR3109928A1/fr
Application granted granted Critical
Publication of FR3109928B1 publication Critical patent/FR3109928B1/fr
Priority to US17/986,149 priority patent/US20230141652A1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • 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
    • 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
    • B64G1/643—Interstage or payload connectors for arranging multiple satellites in a single launcher
    • 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
    • B64G1/645—Separators

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Clamps And Clips (AREA)
  • Toys (AREA)

Abstract

Dispositif de déploiement amélioré pour nano-satellite L’invention concerne un dispositif de déploiement (1) d’un nano-satellite (5) comprenant une structure principale (2) montée sur un lanceur, un cadre de support (3) portant le nano-satellite (5), une structure de verrouillage/déverrouillage (4), le dispositif de déploiement (1) étant caractérisé en ce que la structure de verrouillage/déverrouillage (4) comprend un premier élément de bridage (41) complémentaire d’un deuxième élément de bridage (42) du cadre de support (3), et un élément d’actionnement (43) élastiquement déformable pour permettre : dans une position de verrouillage, de contraindre le premier élément de bridage (41) au deuxième élément de bridage (42) afin de retenir le cadre de support (3) à la structure principale (2), et dans une position de déverrouillage, de libérer le premier élément de bridage (41) du deuxième élément de bridage (42) afin de libérer le cadre de support (3) de la structure principale (2) pour son éjection. Figure de l’abrégé : Fig.3
FR2004623A 2020-05-11 2020-05-11 Dispositif de déploiement amélioré pour nano-satellite Active FR3109928B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR2004623A FR3109928B1 (fr) 2020-05-11 2020-05-11 Dispositif de déploiement amélioré pour nano-satellite
EP21731253.7A EP4149841A1 (fr) 2020-05-11 2021-05-11 Dispositif de déploiement amélioré pour nano-satellite
PCT/FR2021/050818 WO2021229178A1 (fr) 2020-05-11 2021-05-11 Dispositif de déploiement amélioré pour nano-satellite
US17/986,149 US20230141652A1 (en) 2020-05-11 2022-11-14 Deployment device for nano-satellite

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2004623A FR3109928B1 (fr) 2020-05-11 2020-05-11 Dispositif de déploiement amélioré pour nano-satellite
FR2004623 2020-05-11

Publications (2)

Publication Number Publication Date
FR3109928A1 FR3109928A1 (fr) 2021-11-12
FR3109928B1 true FR3109928B1 (fr) 2022-04-22

Family

ID=72088265

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2004623A Active FR3109928B1 (fr) 2020-05-11 2020-05-11 Dispositif de déploiement amélioré pour nano-satellite

Country Status (4)

Country Link
US (1) US20230141652A1 (fr)
EP (1) EP4149841A1 (fr)
FR (1) FR3109928B1 (fr)
WO (1) WO2021229178A1 (fr)

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3467745D1 (en) * 1983-03-03 1988-01-07 Fokker Aircraft System for breaking a tensioned connecting element
US5125601A (en) * 1991-12-26 1992-06-30 The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Payload retention device
US6227493B1 (en) * 1999-04-06 2001-05-08 Planetary Systems Corporation Reusable, separable, structural connector assembly
SE0003315L (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
US20050279890A1 (en) * 2004-03-23 2005-12-22 Walter Holemans Latching separation system
US7748663B1 (en) * 2005-05-24 2010-07-06 Lockheed Martin Corporation Launch vehicle stage integration device
US7905453B2 (en) * 2006-12-21 2011-03-15 Intelsat Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary
US8979035B2 (en) * 2009-11-18 2015-03-17 Ruag Schweiz Ag Zero-shock separation system
US9180984B2 (en) * 2012-05-11 2015-11-10 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
US8915472B2 (en) * 2012-05-11 2014-12-23 The Boeing Company Multiple space vehicle launch system
US9707748B2 (en) * 2013-10-07 2017-07-18 Planetary Systems Corporation Printed spacecraft separation system
EP3145812A4 (fr) * 2014-05-19 2018-01-24 MacDonald, Dettwiler and Associates Inc. Système d'éjection de charges utiles
EP3012194B1 (fr) * 2014-10-24 2020-07-08 Thales Manipulation d'un satellite dans l'espace
US10633896B1 (en) * 2015-03-17 2020-04-28 Raul Barba Theft resistant locking device for a roll-up door
FR3041609B1 (fr) * 2015-09-30 2017-09-08 Airbus Defence & Space Sas Dispositif de separation controlee entre deux pieces et application d'un tel dispositif
CN106742081B (zh) * 2016-11-29 2021-02-05 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
US10669048B1 (en) * 2017-06-15 2020-06-02 United Launch Alliance, L.L.C. Mechanism for increasing jettison clearance

Also Published As

Publication number Publication date
WO2021229178A1 (fr) 2021-11-18
EP4149841A1 (fr) 2023-03-22
US20230141652A1 (en) 2023-05-11
FR3109928A1 (fr) 2021-11-12

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