DE60204836D1 - Pyrotechnic separation device and thus equipped separation system - Google Patents

Pyrotechnic separation device and thus equipped separation system

Info

Publication number
DE60204836D1
DE60204836D1 DE60204836T DE60204836T DE60204836D1 DE 60204836 D1 DE60204836 D1 DE 60204836D1 DE 60204836 T DE60204836 T DE 60204836T DE 60204836 T DE60204836 T DE 60204836T DE 60204836 D1 DE60204836 D1 DE 60204836D1
Authority
DE
Germany
Prior art keywords
separation
pyrotechnic
separation device
separation system
pyrotechnic separation
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
DE60204836T
Other languages
German (de)
Other versions
DE60204836T2 (en
Inventor
Bernard Louis Martin
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.)
Dassault Aviation SA
Original Assignee
Dassault Aviation SA
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 Dassault Aviation SA filed Critical Dassault Aviation SA
Application granted granted Critical
Publication of DE60204836D1 publication Critical patent/DE60204836D1/en
Publication of DE60204836T2 publication Critical patent/DE60204836T2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • F42B15/38—Ring-shaped explosive elements for the separation of rocket parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Insulating Bodies (AREA)
  • Air Bags (AREA)
  • Details Of Connecting Devices For Male And Female Coupling (AREA)
DE2002604836 2001-12-14 2002-12-12 Pyrotechnic separation device and thus equipped separation system Expired - Lifetime DE60204836T2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0116196A FR2833694B1 (en) 2001-12-14 2001-12-14 PYROTECHNIC SEPARATOR AND SEPARATING DEVICE EQUIPPED WITH SUCH A SEPARATOR
FR0116196 2001-12-14

Publications (2)

Publication Number Publication Date
DE60204836D1 true DE60204836D1 (en) 2005-08-04
DE60204836T2 DE60204836T2 (en) 2006-01-12

Family

ID=8870500

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2002604836 Expired - Lifetime DE60204836T2 (en) 2001-12-14 2002-12-12 Pyrotechnic separation device and thus equipped separation system

Country Status (4)

Country Link
EP (1) EP1319920B1 (en)
DE (1) DE60204836T2 (en)
ES (1) ES2243674T3 (en)
FR (1) FR2833694B1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005030090B4 (en) 2005-06-27 2007-03-22 Diehl Bgt Defence Gmbh & Co. Kg Throw-off hood and missile with detachable hood
FR2957143B1 (en) * 2010-03-02 2012-05-04 Astrium Sas PYROTECHNIC RUPTURE CONNECTION DEVICE
DE102012110450B4 (en) * 2012-10-31 2014-07-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Object for a mission into space
US10940341B2 (en) 2013-03-06 2021-03-09 Airbus Canada Limited Partnership Interface between fire suppressant conduit and cargo compartment of an aircraft
FR3028608B1 (en) 2014-11-19 2017-05-05 Dassault Aviat PYROTECHNIC SEPARATOR COMPRISING A SHOCK ABSORPTION MEMBER
FR3028609B1 (en) 2014-11-19 2017-05-05 Dassault Aviat PYROTECHNIC SEPARATOR COMPRISING TWO INDEPENDENT STRUCTURAL ELEMENTS ASSEMBLED TO ONE ANOTHER, AND PROCESS FOR MANUFACTURING THE SAME
US10934029B2 (en) * 2017-05-04 2021-03-02 Paragon Space Development Corporation Thermally isolating joint assembly in a space vehicle
CN113566659B (en) * 2020-04-29 2024-01-16 大连理工大学 Transverse-longitudinal separation integrated interstage line type separation device and application thereof
US11572203B2 (en) * 2021-07-08 2023-02-07 Saab Bofors Dynamics Switzerland Ltd. Release mechanism

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3427047A (en) * 1966-11-30 1969-02-11 Nasa Tubular coupling having frangible connecting means
US3453960A (en) * 1967-12-11 1969-07-08 Gen Dynamics Corp Noncontaminating linear explosive separation
US3633456A (en) * 1969-07-03 1972-01-11 Mc Donnell Douglas Corp Power-actuated separation system
US3698281A (en) 1970-02-27 1972-10-17 Lockheed Aircraft Corp Explosive system
US6298786B1 (en) * 1997-12-16 2001-10-09 Lockheed Martin Corporation Frangible access panel system

Also Published As

Publication number Publication date
FR2833694B1 (en) 2006-02-03
DE60204836T2 (en) 2006-01-12
EP1319920B1 (en) 2005-06-29
ES2243674T3 (en) 2005-12-01
FR2833694A1 (en) 2003-06-20
EP1319920A1 (en) 2003-06-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition