AR103496A1 - Dispositivo pasivo para facilitar la desintegración de un sistema espacial durante su reingreso a la atmósfera terrestre - Google Patents

Dispositivo pasivo para facilitar la desintegración de un sistema espacial durante su reingreso a la atmósfera terrestre

Info

Publication number
AR103496A1
AR103496A1 ARP150103923A ARP150103923A AR103496A1 AR 103496 A1 AR103496 A1 AR 103496A1 AR P150103923 A ARP150103923 A AR P150103923A AR P150103923 A ARP150103923 A AR P150103923A AR 103496 A1 AR103496 A1 AR 103496A1
Authority
AR
Argentina
Prior art keywords
space system
entry
passive device
facilitate
disintegration
Prior art date
Application number
ARP150103923A
Other languages
English (en)
Inventor
Nebiolo Marco
Grasi Lilith
Gennaro Corrado
Destefanis Roberto
Attina Primo
Parissenti Guido
Original Assignee
Thales Alenia Space Italia Spa Con Unico Socio
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 Thales Alenia Space Italia Spa Con Unico Socio filed Critical Thales Alenia Space Italia Spa Con Unico Socio
Publication of AR103496A1 publication Critical patent/AR103496A1/es

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
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
    • 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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1021—Earth observation satellites
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B31/00—Screwed connections specially modified in view of tensile load; Break-bolts
    • F16B31/007—Break-bolts loosening at high temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Tents Or Canopies (AREA)
  • Catching Or Destruction (AREA)
  • Casings For Electric Apparatus (AREA)
  • Sewage (AREA)
  • Emergency Protection Circuit Devices (AREA)

Abstract

Sistema espacial (1) que comprende una estructura (2) formada por componentes estructurales (3), un equipamiento a bordo (5) portado por la estructura (2) y un dispositivo pasivo diseñado para facilitar la destrucción del sistema espacial (1) durante la reentrada a la atmósfera terrestre. El dispositivo pasivo comprende miembros de conexión (4) diseñados para conectar de modo estable los componentes estructurales (3). Los miembros de conexión (4) comprenden al menos una porción hecha de un material iniciador con características tales como para desintegrarse a altitudes de reentrada mayores que aquellas en las que los miembros de conexión actuales se funden, de modo de hacer inestable la conexión creada por los miembros de conexión (4) hasta tal punto como para disparar la destrucción temprana de la estructura (2) del sistema espacial (1) durante la reentrada a la atmósfera terrestre.
ARP150103923A 2014-12-01 2015-12-01 Dispositivo pasivo para facilitar la desintegración de un sistema espacial durante su reingreso a la atmósfera terrestre AR103496A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO20140998 2014-12-01

Publications (1)

Publication Number Publication Date
AR103496A1 true AR103496A1 (es) 2017-05-17

Family

ID=52444563

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP150103923A AR103496A1 (es) 2014-12-01 2015-12-01 Dispositivo pasivo para facilitar la desintegración de un sistema espacial durante su reingreso a la atmósfera terrestre

Country Status (13)

Country Link
US (1) US10589880B2 (es)
EP (1) EP3227184B1 (es)
JP (1) JP6723241B2 (es)
KR (1) KR102431702B1 (es)
CN (1) CN107000853B (es)
AR (1) AR103496A1 (es)
BR (1) BR112017011602A2 (es)
CA (1) CA2969181C (es)
EA (1) EA037450B1 (es)
ES (1) ES2784899T3 (es)
IL (1) IL252541B (es)
TW (1) TW201627202A (es)
WO (1) WO2016088044A1 (es)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3145812A4 (en) * 2014-05-19 2018-01-24 MacDonald, Dettwiler and Associates Inc. Payload ejection system
DE102016205326A1 (de) * 2016-03-31 2017-10-05 Airbus Ds Gmbh Thermisch fragmentierbare Befestigungseinrichtung
DE102016212582A1 (de) * 2016-07-11 2018-01-11 Airbus Ds Gmbh Verbindungsanordnung für einen Satelliten mit wärmegesteuertem Sollbruchverhalten
US10538341B1 (en) 2018-07-06 2020-01-21 Vector Launch Inc. Self-mating modular satellite bus
US10689131B2 (en) * 2018-07-06 2020-06-23 Lockheed Martin Corporation Sectioned self-mating modular satellite buses
EP3604143B1 (en) * 2018-07-30 2021-10-27 European Space Agency Exothermic reaction aided spacecraft demise during re-entry
US10377510B1 (en) 2018-11-14 2019-08-13 Vector Launch Inc. Enhanced fairing mechanisms for launch systems
JP7464937B2 (ja) * 2019-05-13 2024-04-10 本田技研工業株式会社 飛翔体
DE102020132644A1 (de) 2020-12-08 2022-06-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verbesserung der Zerstörbarkeit während des atmosphärischen Eintritts-Flugs durch Beschichtung von Bauteil-Oberflächen
EP4361047A1 (en) * 2022-10-31 2024-05-01 Airbus Defence and Space GmbH Two-part passive separation mechanism for separation of two spacecraft components during the atmospheric re-entry of the spacecraft

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5119555A (en) * 1988-09-19 1992-06-09 Tini Alloy Company Non-explosive separation device
US5695306A (en) * 1996-05-08 1997-12-09 Lockheed Martin Corp. Fusible member connection apparatus and method
US6357699B1 (en) * 2000-05-25 2002-03-19 The Boeing Company Device for controlled release of tension
ES2188331B1 (es) * 2000-09-20 2004-06-16 Sener, Ingenieria Y Sistemas, S.A. Mecanismo de amarre y liberacion de equipos con actuacion remota.
US6895314B2 (en) * 2003-06-11 2005-05-17 The Aerospace Corporation Spacecraft reentry breakup recorder
US7290737B2 (en) * 2005-09-29 2007-11-06 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Nonsurvivable momentum exchange system
JP5448544B2 (ja) * 2009-04-17 2014-03-19 三菱重工業株式会社 宇宙機用複合材料及び燃料タンク
FR2959490B1 (fr) * 2010-04-28 2012-07-13 Astrium Sas Satellite a structure simplifiee, allegee et economique, et son procede de mise en oeuvre
WO2014045078A1 (en) * 2012-09-21 2014-03-27 Agence Spatiale Europeenne Re-entry broadcasting alert apparatus, system and method

Also Published As

Publication number Publication date
JP6723241B2 (ja) 2020-07-15
TW201627202A (zh) 2016-08-01
IL252541B (en) 2021-04-29
CN107000853A (zh) 2017-08-01
EA037450B1 (ru) 2021-03-30
US20170327251A1 (en) 2017-11-16
EP3227184B1 (en) 2020-01-29
ES2784899T3 (es) 2020-10-01
CA2969181A1 (en) 2016-06-09
JP2017536294A (ja) 2017-12-07
WO2016088044A1 (en) 2016-06-09
EP3227184A1 (en) 2017-10-11
KR20170110577A (ko) 2017-10-11
CA2969181C (en) 2022-08-16
BR112017011602A2 (pt) 2018-03-06
CN107000853B (zh) 2020-07-10
IL252541A0 (en) 2017-07-31
KR102431702B1 (ko) 2022-08-11
EA201791205A1 (ru) 2017-10-31
US10589880B2 (en) 2020-03-17

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