BR112017011602A2 - dispositivo passivo projetado para facilitar a desintegração de um sistema espacial durante a reentrada na atmosfera da terra - Google Patents

dispositivo passivo projetado para facilitar a desintegração de um sistema espacial durante a reentrada na atmosfera da terra

Info

Publication number
BR112017011602A2
BR112017011602A2 BR112017011602A BR112017011602A BR112017011602A2 BR 112017011602 A2 BR112017011602 A2 BR 112017011602A2 BR 112017011602 A BR112017011602 A BR 112017011602A BR 112017011602 A BR112017011602 A BR 112017011602A BR 112017011602 A2 BR112017011602 A2 BR 112017011602A2
Authority
BR
Brazil
Prior art keywords
space system
entry
earth
atmosphere
disintegration
Prior art date
Application number
BR112017011602A
Other languages
English (en)
Inventor
Gennaro Corrado
Parissenti Guido
Grassi Lilith
Nebiolo Marco
Attina' Primo
Destefanis Roberto
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 BR112017011602A2 publication Critical patent/BR112017011602A2/pt

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)
  • Casings For Electric Apparatus (AREA)
  • Sewage (AREA)
  • Emergency Protection Circuit Devices (AREA)
  • Catching Or Destruction (AREA)

Abstract

é descrito um sistema espacial (1), compreendendo uma estrutura (2) formada por componentes estruturais (3), um equipamento de bordo (5) transportado pela estrutura (2), e um dispositivo passivo concebido para facilitar a desintegração e o desaparecimento do sistema espacial (1) durante a reentrada na atmosfera da terra. o dispositivo passivo compreende membros de conexão (4) concebidos para conectarem de forma estável os componentes estruturais (3). os membros de conexão (4) compreendem pelo menos uma porção feita de um material de desencadeamento tendo características de degradação a altitudes de reentrada mais elevadas do que aquelas nas quais os elementos de conexão atuais se derretem, de modo a tornar instável a conexão criada pelos membros de conexão (4), para desencadear a desintegração prematura da estrutura (2) do sistema espacial (1) durante a reentrada na atmosfera terrestre.
BR112017011602A 2014-12-01 2015-12-01 dispositivo passivo projetado para facilitar a desintegração de um sistema espacial durante a reentrada na atmosfera da terra BR112017011602A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITTO20140998 2014-12-01
PCT/IB2015/059257 WO2016088044A1 (en) 2014-12-01 2015-12-01 Passive device designed to facilitate demise of a space system during re-entry into the earth's atmosphere

Publications (1)

Publication Number Publication Date
BR112017011602A2 true BR112017011602A2 (pt) 2018-03-06

Family

ID=52444563

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017011602A BR112017011602A2 (pt) 2014-12-01 2015-12-01 dispositivo passivo projetado para facilitar a desintegração de um sistema espacial durante a reentrada na atmosfera da terra

Country Status (13)

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

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2946333C (en) * 2014-05-19 2020-12-08 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
US10689131B2 (en) * 2018-07-06 2020-06-23 Lockheed Martin Corporation Sectioned self-mating modular satellite buses
US10538341B1 (en) 2018-07-06 2020-01-21 Vector Launch Inc. Self-mating modular satellite bus
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
US10589880B2 (en) 2020-03-17
EA037450B1 (ru) 2021-03-30
US20170327251A1 (en) 2017-11-16
CA2969181C (en) 2022-08-16
KR102431702B1 (ko) 2022-08-11
KR20170110577A (ko) 2017-10-11
JP2017536294A (ja) 2017-12-07
AR103496A1 (es) 2017-05-17
WO2016088044A1 (en) 2016-06-09
EP3227184A1 (en) 2017-10-11
IL252541A0 (en) 2017-07-31
IL252541B (en) 2021-04-29
EP3227184B1 (en) 2020-01-29
CA2969181A1 (en) 2016-06-09
CN107000853B (zh) 2020-07-10
ES2784899T3 (es) 2020-10-01
JP6723241B2 (ja) 2020-07-15
EA201791205A1 (ru) 2017-10-31
TW201627202A (zh) 2016-08-01
CN107000853A (zh) 2017-08-01

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]
B12B Appeal against refusal [chapter 12.2 patent gazette]