EA201791205A1 - Пассивное устройство, выполненное с возможностью способствования прекращению существования космической системы во время входа в атмосферу земли - Google Patents

Пассивное устройство, выполненное с возможностью способствования прекращению существования космической системы во время входа в атмосферу земли

Info

Publication number
EA201791205A1
EA201791205A1 EA201791205A EA201791205A EA201791205A1 EA 201791205 A1 EA201791205 A1 EA 201791205A1 EA 201791205 A EA201791205 A EA 201791205A EA 201791205 A EA201791205 A EA 201791205A EA 201791205 A1 EA201791205 A1 EA 201791205A1
Authority
EA
Eurasian Patent Office
Prior art keywords
space system
existence
earth
passive device
possibility
Prior art date
Application number
EA201791205A
Other languages
English (en)
Other versions
EA037450B1 (ru
Inventor
Гвидо Париссенти
Примо Аттина
Роберто Дестефанис
Коррадо Дженнаро
Лилит Грасси
Марко Небиоло
Original Assignee
Таль Аления Спейс Италия С.П.А. Кон Унико Сочио
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 Таль Аления Спейс Италия С.П.А. Кон Унико Сочио filed Critical Таль Аления Спейс Италия С.П.А. Кон Унико Сочио
Publication of EA201791205A1 publication Critical patent/EA201791205A1/ru
Publication of EA037450B1 publication Critical patent/EA037450B1/ru

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

Космическая система (1) содержит структуру (2), сформированную посредством структурных компонентов (3), бортовое оборудование (5), поддерживаемое посредством структуры (2), и пассивное устройство, выполненное с возможностью способствования прекращению существования космической системы (1) во время входа в атмосферу Земли. Пассивное устройство содержит соединительные элементы (4), выполненные с возможностью устойчивого соединения структурных компонентов (3). Соединительные элементы (4) содержат, по меньшей мере, фрагмент, выполненный из инициирующего материала с такими характеристиками, чтобы разрушаться на высотах входа в атмосферу выше высот, на которых текущие соединительные элементы плавятся, с тем, чтобы делать неустойчивым соединение, сформированное посредством соединительных элементов (4), до такой степени, чтобы раньше инициировать прекращение существования структуры (2) космической системы (1) во время входа в атмосферу Земли.
EA201791205A 2014-12-01 2015-12-01 Пассивное устройство инициирования распада космической системы на части во время входа в атмосферу земли EA037450B1 (ru)

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 (2)

Publication Number Publication Date
EA201791205A1 true EA201791205A1 (ru) 2017-10-31
EA037450B1 EA037450B1 (ru) 2021-03-30

Family

ID=52444563

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201791205A EA037450B1 (ru) 2014-12-01 2015-12-01 Пассивное устройство инициирования распада космической системы на части во время входа в атмосферу земли

Country Status (13)

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

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
AR103496A1 (es) 2017-05-17
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
US10589880B2 (en) 2020-03-17

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