AU2001252824A1 - Device and method for connecting two parts of a craft - Google Patents

Device and method for connecting two parts of a craft

Info

Publication number
AU2001252824A1
AU2001252824A1 AU2001252824A AU5282401A AU2001252824A1 AU 2001252824 A1 AU2001252824 A1 AU 2001252824A1 AU 2001252824 A AU2001252824 A AU 2001252824A AU 5282401 A AU5282401 A AU 5282401A AU 2001252824 A1 AU2001252824 A1 AU 2001252824A1
Authority
AU
Australia
Prior art keywords
craft
parts
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.)
Abandoned
Application number
AU2001252824A
Inventor
Ingvar Bengtsson
Bengt Mortberg
Shawn H. Smith
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.)
RUAG Space AB
Original Assignee
SAAB Ericson Space AB
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 SAAB Ericson Space AB filed Critical SAAB Ericson Space AB
Publication of AU2001252824A1 publication Critical patent/AU2001252824A1/en
Abandoned legal-status Critical Current

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
    • B64G1/645—Separators
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Clamps And Clips (AREA)
AU2001252824A 2000-05-10 2001-04-20 Device and method for connecting two parts of a craft Abandoned AU2001252824A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09568144 2000-05-10
US09/568,144 US6454214B1 (en) 2000-05-10 2000-05-10 Device and method for connecting two parts of a craft
PCT/SE2001/000906 WO2001085542A1 (en) 2000-05-10 2001-04-20 Device and method for connecting two parts of a craft

Publications (1)

Publication Number Publication Date
AU2001252824A1 true AU2001252824A1 (en) 2001-11-20

Family

ID=24270076

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001252824A Abandoned AU2001252824A1 (en) 2000-05-10 2001-04-20 Device and method for connecting two parts of a craft

Country Status (4)

Country Link
US (1) US6454214B1 (en)
EP (1) EP1339604B1 (en)
AU (1) AU2001252824A1 (en)
WO (1) WO2001085542A1 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE0003315L (en) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Device and method for a spacecraft
US6712542B2 (en) * 2002-01-15 2004-03-30 The Boeing Company Apparatus and method for altering the tension of a clampband
DE10301783B4 (en) * 2003-01-18 2005-04-28 Eads Space Transp Gmbh Device for releasably connecting rotationally symmetrical components
ES2372060T3 (en) * 2005-10-06 2012-01-13 Eads Casa Espacio, S.L. CONNECTION-SEPARATION DEVICE OF A LAUNCHER VEHICLE AND A SATELLITE.
US7686529B1 (en) 2007-12-18 2010-03-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Two-axis joint assembly and method
US8082848B2 (en) * 2008-10-22 2011-12-27 Raytheon Company Missile with system for separating subvehicles
US8979035B2 (en) * 2009-11-18 2015-03-17 Ruag Schweiz Ag Zero-shock separation system
JP5479145B2 (en) 2010-02-18 2014-04-23 三菱重工業株式会社 Bond separation device, bond separation system, and bond separation method
JP5479146B2 (en) * 2010-02-19 2014-04-23 三菱重工業株式会社 Bond separation device, bond separation system, and bond separation method
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
CN102767996B (en) * 2012-07-30 2014-08-27 上海宇航系统工程研究所 Low-impact clamp band joint unlocking device
US10190537B2 (en) 2013-07-02 2019-01-29 Mra Systems, Inc. Engine and band clamp
EP3448758B1 (en) * 2016-04-25 2021-03-31 RUAG Space AB Separable roller screw assembly for a space craft release mechanism system
EP3478586A4 (en) 2016-06-30 2020-02-19 RUAG Space AB Joint and clamp band system for releasably connecting space craft elements
US11247788B2 (en) * 2016-12-22 2022-02-15 Airbus Defence and Space S.A. Connection/separation device for separating satellites from shuttles or from satellite dispensers
US10669048B1 (en) * 2017-06-15 2020-06-02 United Launch Alliance, L.L.C. Mechanism for increasing jettison clearance
US11472577B2 (en) 2019-09-26 2022-10-18 Jeanette Ann Houghton Near zero shock bolt catcher assembly
WO2024018092A1 (en) * 2022-07-19 2024-01-25 Airbus Defence And Space, S.A. Bolt release system for spacecraft and launcher separation systems and separation system comprising same

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2967482A (en) * 1958-11-21 1961-01-10 Jr John B Toomey Release mechanism
US3122098A (en) * 1960-11-25 1964-02-25 Glennan Thomas Keith Apparatus and method for control of a solid fueled rocket vehicle
US3109216A (en) * 1960-12-29 1963-11-05 Hi Shear Corp Explosively separable bolt and clamp
US3404649A (en) * 1967-02-16 1968-10-08 Navy Usa Ballast configuration and release concept
US4715565A (en) * 1986-05-27 1987-12-29 Hughes Aircraft Company Clamping connection assembly for spacecraft
FR2670844B1 (en) 1990-12-21 1993-04-16 Aerospatiale REMOTE RELEASE TENSIONING MECHANISM OF A FLEXIBLE MEMBER SUCH AS A STRAP AND DEVICE FOR RIGID CONNECTION OF TWO MECHANICAL ASSEMBLIES USING SUCH A MECHANISM.
US5318255A (en) * 1992-06-22 1994-06-07 Hughes Aircraft Company Stage separation mechanism for space vehicles
US5603595A (en) 1995-04-12 1997-02-18 Martin Marietta Corp. Flywheel nut separable connector and method
ES2131476B1 (en) 1997-09-26 2000-03-01 Const Aeronauticas Sa SATELLITE FIXING AND SEPARATION SYSTEM.
WO2001002248A1 (en) 1999-07-02 2001-01-11 Saab Ericsson Space Ab Method and device for the separation of a satellite from a carrier rocket

Also Published As

Publication number Publication date
US6454214B1 (en) 2002-09-24
EP1339604B1 (en) 2005-11-30
EP1339604A1 (en) 2003-09-03
WO2001085542A1 (en) 2001-11-15

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